MICRO LABSAT

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite MICRO LABSAT at a glance.

Uptime

8240

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: 100.652 minutes

Inclination: 98.7608 deg

SMA: 7167.639 km

Apoapsis: 796.376 km

Periapsis: 782.632 km

RAAN: 144.4626 deg

Eccentricy: 0.0009588

Argument of periapsis: 240.9544 deg

Mean anomaly: 119.0678 deg

Mean motion: 14.30667015 rev/day

Mean motion (dot): 0.00000104 rev/day2

B* drag term: 0.000057048 1/REarth

Two-line elements (TLE)

Creation date: July 5, 2025, 5:45 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 5, 2025, 11:49 a.m. UTC

TLE line 0: 0 MICRO LABSAT

TLE line 1: 1 27600U 02056D 25186.49261508 .00000104 00000-0 57048-4 0 9998

TLE line 2: 2 27600 98.7608 144.4626 0009588 240.9544 119.0678 14.30667015176964

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.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB LEO 2025-06-12 04:35:08 0.0002271955 581.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-01-31 16:02:03 0.000165614 784.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-06-23 18:37:00 0.0002020353 800.0 (m) DEBRIS
DMSP 5D-2 F13 DEB SSO 2024-06-18 14:27:22 0.0001045977 318.0 (m) DEBRIS
ARIANE 1 DEB SSO 2024-05-27 21:05:31 0.001387054 195.0 (m) DEBRIS

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.

Launch to space H-IIA 202 | Midori-2
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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