Key statistics
Satellite ADEOS 2 at a glance.
Uptime
8299
Days in orbit
Revolutions
≈ 14.3
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
Latest
Satellite identification and parameters
Extended collection of information and parameters for ADEOS 2.
Object identification
Identified? True
Debris? False
Object name: ADEOS 2
International designator: 2002-056A
Object number (NORAD): 27597
Object ID (CCSDS): 27597
Country: JAPAN (JPN)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 100.763 minutes
Inclination: 98.7442 deg
SMA: 7172.877 km
Apoapsis: 795.697 km
Periapsis: 793.787 km
RAAN: 198.3583 deg
Eccentricy: 0.00013317
Argument of periapsis: 129.7401 deg
Mean anomaly: 230.3898 deg
Mean motion: 14.29100267 rev/day
Mean motion (dot): 0.0000061 rev/day2
B* drag term: 0.00025853758 1/REarth
Two-line elements (TLE)
Creation date: Sept. 3, 2025, 2:21 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 2, 2025, 7:53 p.m. UTC
TLE line 0: 0 ADEOS 2
TLE line 1: 1 27597U 02056A 25245.82914437 .00000610 00000-0 25854-3 0 9993
TLE line 2: 2 27597 98.7442 198.3583 0001332 129.7401 230.3898 14.29100267183463
Live tracking on map
Real-time ground track for satellite ADEOS 2.
In-orbit conjunctions
A list of the most updated potential collisions computed for object ADEOS 2.
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.
ADEOS 2 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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