Key statistics
Satellite FEDSAT at a glance.
Uptime
8299
Days in orbit
Revolutions
≈ 14.3
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.8
Latest
Satellite identification and parameters
Extended collection of information and parameters for FEDSAT.
Object identification
Identified? True
Debris? False
Object name: FEDSAT
International designator: 2002-056B
Object number (NORAD): 27598
Object ID (CCSDS): 27598
Country: AUSTRALIA (AUS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 100.728 minutes
Inclination: 98.8168 deg
SMA: 7171.218 km
Apoapsis: 800.32 km
Periapsis: 785.846 km
RAAN: 209.6565 deg
Eccentricy: 0.00100919
Argument of periapsis: 95.4903 deg
Mean anomaly: 264.743 deg
Mean motion: 14.29596086 rev/day
Mean motion (dot): 0.00000349 rev/day2
B* drag term: 0.0001542803 1/REarth
Two-line elements (TLE)
Creation date: Sept. 2, 2025, 11:42 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 2, 2025, 12:42 p.m. UTC
TLE line 0: 0 FEDSAT
TLE line 1: 1 27598U 02056B 25245.52942682 .00000349 00000-0 15428-3 0 9999
TLE line 2: 2 27598 98.8168 209.6565 0010092 95.4903 264.7430 14.29596086184658
Live tracking on map
Real-time ground track for satellite FEDSAT.
In-orbit conjunctions
A list of the most updated potential collisions computed for object FEDSAT.
Associated space launch
Midori II has been engaged in various observation missions to understand the realities and causes of global environmental changes, such as abnormal weather conditions and the expansion of the ozone hole.
FEDSAT was lifted into orbit during the mission ‘H-IIA 202 | Midori-2’, on board a H-IIA space rocket.
The launch took place on Dec. 14, 2002, 1:31 a.m. from Yoshinobu Launch Complex LP-1.
For more information about the launch, click the button.

H-IIA 202 | Midori-2
Agency: N/A
Status: Launch Successful
Launch date: Dec. 14, 2002, 1:31 a.m. UTC
Rocket: H-IIA
Launch pad: Yoshinobu Launch Complex LP-1
Location: Tanegashima Space Center, Japan
...
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