As our space activities expand, the number of satellites and space debris orbiting around the Earth continues to grow, increasing the risk of collision of such space objects.

Satellites are now an indispensable infrastructure to support our daily life, including weather forecasts by meteorological satellites, TV programs via broadcasting satellites, and car navigation system by positioning satellites. It is imperative to be aware of the orbits of space objects, such as space debris, and maintain a catalog of these objects for the stable use of space, that is, Space Situational Awareness (SSA).


Space debris is defined as all non-functional, human-made objects in Earth orbit such as:

  • ・Inactive satellites
  • ・Upper stages and fragments of launch vehicles
  • ・Fragments created by fuel tank explosions or intentional destruction
  • ・Fragments caused by collisions of space debris

Space Debris is Steadily Increasing

Since space activities started around 1956, the number of space debris has been continuously increasing. According to a catalogue published by the US Combined Space Operations Center (CSpOC) which contains space objects up to softball-sized, there are almost 20,000 objects orbiting around the Earth, while the actual number is thought to be more.

The Risks of Space Debris

If space debris collides with an operational satellite or the International Space Station, it can damage or ruin the spacecraft as well as become threats to the lives of astronauts. Once a collision occurs, fragments generated from the collision also become space debris and increase its total number. Most of such objects on lower orbits will eventually re-enter the atmosphere and burn down. But some of them would fall to the ground without burning down, which can cause catastrophic damage to the area.


JAXA has been taking various measures to tackle space debris problems, including SSA activities by Space Tracking and Communications Center (STCC) such as observation and analysis of space debris, as follows:

Observation: Technology to observe space debris on Earth's orbit
Analysis: Technology to calculate the probability of collision of space debris with operational satellites, and to predict how space debris will increase in the future
Protection: Technology to protect spacecraft from fatal damage even if a collision occurs
Prevention: Technologies to prevent space debris from increasing, and to remove space debris from near-Earth region.

see here for SSA activities other than observation.

SSA Activities

In the 1980s, JAXA conducted joint research with the National Astronomical Observatory of Japan (NAOJ) to observe space objects using NAOJ’s telescopes. In the 2000s, JAXA started developing technologies including analyzing such objects by utilizing observation data acquired at Bisei Space Guard Center (optical telescopes) and Kamisaibara Space Guard Center (radar), both built by the Japan Space Forum. In April 2017, these telescope and radar facilities were transferred to JAXA for the SSA activities expected to gain more importance. Both facilities will be renewed by 2023.

Distribution of Space Debris

The 70% of space debris that can be observed from the ground are distributed on low orbit (its altitude is lower than 2,000 km), and the rest is around higher altitudes such as geostationary orbit (36,000 km). JAXA observes space debris on low orbit using its radar system, and those on geostationary orbit by utilizing its optical telescopes.

Distribution of Space Debris

JAXA’s SSA System Configuration

The JAXA SSA system consists of the radar to observe space debris on low orbit, the optical telescopes to observe space debris on geostationary orbit, and the analysis system to calculate their orbits and do further analysis based on data obtainded from thsese facilities.



The JAXA SSA system is composed of a radar at Kamisaibara Space Guard Center in Kagamino-cho and optical telescopes at Bisei Space Guard Center in Ibara-shi, both located in Okayama, as well as an analysis system at the STCC in Tsukuba Space Center in Ibaraki.

Space Debris Observation Facilities
The Kamisaibara Space Guard Center uses radar Bisei Space-Guard Center uses optical telescopes.


The radar system measures the distance from its radar antenna to a space object by measuring the round-trip time of the radio wave between them. Also, the azimuth and elevation angle of the object with respect to the radar can be calculated by measuring the direction of the reflected radar beam.

The distance is calculated based on the radio wave turnaround time. The angles (azimuth and elevation angle) are calculated based on the irradiation direction of the radio waves.

Low earth orbit space debris observed by the radar are going around the Earth multiple times a day, so the visible time from the radar antenna is limited. Therefore, the radar system collects the distance, azimuth and elevation angle data as much as possible during the limited visible time. The orbit of the space debris is determined using the data.

Multiple Data Items are used to measure the orbit of an object: Distance and angle (azimuth and elevation angle) are the most crucial.


The stars remain fixed on the celestial sphere, whereas the space debris moves. We detect objects moving on the celestial sphere from time-series observation images obtained by optical telescopes, and calculate positions of the object on the celestial sphere (right ascension and declination). Because the precise positions of the guide stars contained in the guide star catalog are known, precise positions of the target objects can be calculated from the relative positions to the guide stars in the field of view.

Calculating the position (right ascension and declination) of the object to be observed on the Celestial Sphere based on time-series observation images

In circular orbits around the Earth, the farther an orbit of object is from the Earth, the slower the transverse velocity of the object is, and the slower the velocity on the celestial sphere (the apparent transverse velocity observed from an observer on the ground) is. On the other hand, the nearer an orbit is to the Earth, the faster the transverse velocity is, and the faster the velocity on the celestial sphere is. Thus, the distance of the object can be estimated from the velocity on the celestial sphere. An orbit of a target object can be determined using a set of position and velocity data at a certain observation time (that can be calculated from an observational data obtained by a single observation) when the object is in a circular orbit. However, it is uncertain if the object is actually in a circular orbit or not. Therefore, a set of observational data obtained at multiple points apart from each other in the orbit is required in the orbit determination process. We perform the orbit determination using observational data at multiple observation times.

Circular Orbit close to Earth, Circular Orbit far from Earth
The orbit can be determined not with only one point, but with two or more points.


The STCC at Tsukuba Space Center uses observation data from the radar and optical telescopes in Okayama prefecture along with information from US CSpOC to perform various analysis. The four main activities we engage at the STCC are as follows:

  • 1) Monitoring to see if space debris is approaching JAXA's satellites.
    By comparing the predicted orbits of our satellites and those of all the catalogued space debris*, we assess if any of space debris is approaching these satellites.
    * Space objects whose orbits are already known.
  • 2) Reporting a possible close approach to an operation team of the satellite.
    Notify and share information on how close and dangerous the space debris can be to the satellite with the operation team.
  • 3) Calculating how the satellite should avoid approaching space debris.
    We assess when, to what direction, and how much the orbit of the satellite should be changed , which is needed for the collision avoidance maneuver.
  • 4) Predicting re-entry of space debris.
    Space objects orbiting around the Earth are slowly lowering their altitudes due to the atmosphere of the Earth and radiation from the Sun, and eventually re-entering the atmosphere. Considering these effects, we predict the orbits of descending space debris and assess when and where the space objects will re-enter the atmosphere.
Space Tracking and Communications Center’s SSA Operations


A national SSA system project is under way and mainly developed by the Ministry of Defense to tackle ever-increasing space debris as an All-Japan initiative. JAXA is planning to contribute to this initiative from a technical point of view with JAXA's new SSA system which is expected to start operating by 2023.

JAXA's new SSA system will have a radar that can track smaller space debris than those the present radar can. The new radar will enable us to understand orbits of more space debris; therefore, we need to upgrade our analysis system to process these increasing observation data. We will refurbish the present optical telescopes. Moreover, the new system has scalabilities for future R&D to enhance space debris observation technologies.

New SSA Radar System

As of 2019, JAXA's operating SSA radar is capable of observing objects, for example, of at least size of 1.6 m in diameter flying at an altitude of 650 km. At the farthest, the radar can observe an object 1,350 kilometers away, but in this case, the size of object must be at least 5.5 m in diameter.
However, many objects smaller than size of 1.6 m are flying around the Earth. Almost 20,000 of such objects, which are so-called “softball size objects”, are cataloged and published by the Combined Space Operation Center (CSpOC). As many as 70% of the objects in the CSpOC catalog exist in the low Earth orbit that JAXA's SSA radar covers, but only about 5% of them can be observed by our current radar.

Therefore, JAXA aims to improve the observation capability of the SSA radar so that we can observe smaller softball (10-cm diameter class) size objects at the altitudes below 650 km. For this purpose, we must improve the observation capability of the radar for more than 200 times.
So, we will increase the size of the radar antenna (increase the number of antenna elements), adopt a semiconductor capable of transmitting longer pulses with a higher output, improve the sensitivity of the receiver, and make improvements not only in hardware but also in software such as signal processing technology.
Details will be provided in the next revision.

(updated in October 2019)

The No. of Space Debris objects published by the CSpOC (Blue)
The No. of Space Debris objects detected using current radar capability (Yellow)
The range and No. of Space Debris objects that will be observable with future SSA radar capability (Orange)

This graph shows the mean altitude distribution of objects that can be observed by JAXA's current radar (yellow) and that of the future SSA radar (orange), in comparison to the number of space debris published by CSpOC as of October 2019 (blue). CSpOC publication includes the number of objects that cannot be observed by JAXA's radar located at Okayama Prefecture.

New SSA Optical Telescope System

As of 2019, JAXA has two SSA optical telescopes: the 1-meter telescope having the primary mirror with a diameter of 1 m and the 50-cm telescope having the primary mirror with a diameter of 50 cm. The observation capability (limiting magnitude) of 1-meter telescope is 18 magnitude and that of the 50-cm telescope is 16.5 magnitude. With this capability, JAXA can observe objects of approximately 1m in diameter around the geostationary orbit (altitude of 36,000km) which is the main observation area for JAXA's SSA optical telescope. Hence, JAXA can observe almost all objects around the geostationary orbit published by CSpOC.

However, current telescopes, especially the 1-meter telescope, began to experience malfunction due to deterioration and other reasons . If this condition persists, there is a risk that observation would become no longer possible. Therefore, we will refurbish the 1-meter telescope to a new one. In addition, we expand the capabilities of both the 1-meter telescope and the 50-cm telescope for the future SSA research and development. Furthermore, we add the functions that enable highly real-time cooperative operations with the analysis system at the Tsukuba Space Center to the data processing system of the telescope. Details will be provided in the next revision.

(updated in October 2019)

As of October 2019, the removal of the old 1-meter telescope has been completed in preparation for the installation of the new 1-meter telescope. The telescope is being tested at the manufacturer's factory before installation and will be transported to the Bisei Space Guard Center for installation After the operation confirmation, the optical telescope system is scheduled to resume operation around spring of 2020.

Click here (Japanese text only) for the factory test (a test to check the movement of a telescope) of the new 1-m telescope. Note that the movement in the movie is 8 times to the real.

New SSA Analysis System (SAKURA)

As the capabilities of JAXA's SSA radar expand, the number of observable objects will increase by nearly 10 times. To respond to this progress, the SSA analysis system that processes the observed data also needs to improve its processing capacity.
In order not to increase the amount of work by increasing the number of objects that can be observed through the development of a new SSA analysis system, we will not only improve the processing capacity but also devise automatic processing as much as possible. The new SSA analysis system will also add a new linkage function to provide observation data to the national SSA system. We plan to create an environment in which new SSA analysis system can be further studied and developed without affecting daily observation operations.
The new SSA analysis system has the nickname "SAKURA" (SsA Key technology Unified Research and Analysis system) meaning cherry blossoms in Japanese.
As in the previous analysis system, SAKURA calculates the orbit of space debris based on the observation data obtained from the radar and the optical telescopes and compares it with the orbits of the JAXA satellites to see if there is no possible close approach. When an approach is detected based on the results of the analysis or information provided by the national SSA system, further analysis is performed to notify the parties concerned under predefined conditions and to provide information necessary for JAXA satellite parties to plan orbit control to avoid space debris collisions.
Also, when an object that JAXA is interested in gradually lowers its altitude is likely to re-enter the atmosphere, an analysis to predict the time and the re-entry point of the atmosphere will be conducted and the necessary information will be notified to the relevant parties.
New feature of SAKURA is the ability to work with the national SSA system. We are devising ways to ensure that observation can be carried out efficiently, taking into account the observation requests not only from JAXA but also from the government.
Details will be provided in the next revision.

(updated in October 2019)

SSA System(Space Situational Awareness)

SSA project team logo
On the left is the silhouette of an optical telescope and on the right is that of a radar. The joyful children in the center depict the safe and peaceful outer space.