Key statistics
Satellite FEDSAT at a glance.
Uptime
8239
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: 100.729 minutes
Inclination: 98.8091 deg
SMA: 7171.286 km
Apoapsis: 798.77 km
Periapsis: 787.531 km
RAAN: 149.2575 deg
Eccentricy: 0.0007836
Argument of periapsis: 271.177 deg
Mean anomaly: 88.8514 deg
Mean motion: 14.29575958 rev/day
Mean motion (dot): 0.00000083 rev/day2
B* drag term: 0.000050379 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 10:36 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 7:52 p.m. UTC
TLE line 0: 0 FEDSAT
TLE line 1: 1 27598U 02056B 25185.82786799 .00000083 00000-0 50379-4 0 9990
TLE line 2: 2 27598 98.8091 149.2575 0007836 271.1770 88.8514 14.29575958176137
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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