Key statistics
Satellite MICRO LABSAT at a glance.
Uptime
8178
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 MICRO LABSAT.
Object identification
Identified? True
Debris? False
Object name: MICRO LABSAT
International designator: 2002-056D
Object number (NORAD): 27600
Object ID (CCSDS): 27600
Country: JAPAN (JPN)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 100.654 minutes
Inclination: 98.7571 deg
SMA: 7167.72 km
Apoapsis: 797.999 km
Periapsis: 781.171 km
RAAN: 82.394 deg
Eccentricy: 0.0011739
Argument of periapsis: 66.2719 deg
Mean anomaly: 293.9694 deg
Mean motion: 14.30642762 rev/day
Mean motion (dot): 0.00000303 rev/day2
B* drag term: 0.00013319 1/REarth
Two-line elements (TLE)
Creation date: May 5, 2025, 2:11 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 4, 2025, 9:03 p.m. UTC
TLE line 0: 0 MICRO LABSAT
TLE line 1: 1 27600U 02056D 25124.87751437 .00000303 00000-0 13319-3 0 9990
TLE line 2: 2 27600 98.7571 82.3940 0011739 66.2719 293.9694 14.30642762168150
Live tracking on map
Real-time ground track for satellite MICRO LABSAT.
In-orbit conjunctions
A list of the most updated potential collisions computed for object MICRO LABSAT.
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.
MICRO LABSAT 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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