MICRO LABSAT

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite MICRO LABSAT 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 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: 100.651 minutes

Inclination: 98.7678 deg

SMA: 7167.561 km

Apoapsis: 797.844 km

Periapsis: 781.007 km

RAAN: 204.3097 deg

Eccentricy: 0.00117458

Argument of periapsis: 71.4281 deg

Mean anomaly: 288.8176 deg

Mean motion: 14.30690537 rev/day

Mean motion (dot): 0.00000397 rev/day2

B* drag term: 0.00016920036 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, 8:51 p.m. UTC

TLE line 0: 0 MICRO LABSAT

TLE line 1: 1 27600U 02056D 25245.86892693 .00000397 00000-0 16920-3 0 9997

TLE line 2: 2 27600 98.7678 204.3097 0011746 71.4281 288.8176 14.30690537185450

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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