WEOS

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite WEOS at a glance.

Uptime

8297

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 WEOS.

Object identification

Identified? True

Debris? False

Object name: WEOS

International designator: 2002-056C

Object number (NORAD): 27599

Object ID (CCSDS): 27599

Country: JAPAN (JPN)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 100.652 minutes

Inclination: 98.7715 deg

SMA: 7167.626 km

Apoapsis: 797.238 km

Periapsis: 781.743 km

RAAN: 203.2236 deg

Eccentricy: 0.00108091

Argument of periapsis: 80.0617 deg

Mean anomaly: 280.1784 deg

Mean motion: 14.30670975 rev/day

Mean motion (dot): 0.00000356 rev/day2

B* drag term: 0.00015344963 1/REarth

Two-line elements (TLE)

Creation date: Sept. 1, 2025, 2:20 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 31, 2025, 8:09 p.m. UTC

TLE line 0: 0 WEOS

TLE line 1: 1 27599U 02056C 25243.84012468 .00000356 00000-0 15345-3 0 9999

TLE line 2: 2 27599 98.7715 203.2236 0010809 80.0617 280.1784 14.30670975184970

Live tracking on map

Real-time ground track for satellite WEOS.

In-orbit conjunctions

A list of the most updated potential collisions computed for object WEOS.

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-04-15 04:26:23 0.0003877345 273.0 (m) DEBRIS
SCOUT A DEB SSO 2025-03-03 17:12:05 0.001306435 514.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-11-25 00:58:11 0.0003712804 814.0 (m) DEBRIS
NOAA 17 DEB SSO 2024-11-08 05:35:11 0.000239232 717.0 (m) DEBRIS
CZ-6A DEB LEO 2024-10-01 13:30:41 0.0008325229 515.0 (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.

WEOS 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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