FEDSAT

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite FEDSAT at a glance.

Uptime

8400

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 FEDSAT.

Object identification

Identified? True

Debris? False

Object name: FEDSAT

International designator: 2002-056B

Object number (NORAD): 27598

Object ID (CCSDS): 27598

Country: AUSTRALIA (AUS)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 100.723 minutes

Inclination: 98.8354 deg

SMA: 7171.014 km

Apoapsis: 799.54 km

Periapsis: 786.217 km

RAAN: 311.6323 deg

Eccentricy: 0.00092888

Argument of periapsis: 156.6333 deg

Mean anomaly: 203.5272 deg

Mean motion: 14.29657314 rev/day

Mean motion (dot): 0.00000263 rev/day2

B* drag term: 0.00012062951 1/REarth

Two-line elements (TLE)

Creation date: Dec. 12, 2025, 10:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 12, 2025, 4:07 a.m. UTC

TLE line 0: 0 FEDSAT

TLE line 1: 1 27598U 02056B 25346.17218150 .00000263 00000-0 12063-3 0 9995

TLE line 2: 2 27598 98.8354 311.6323 0009289 156.6333 203.5272 14.29657314199039

Live tracking on map

Real-time ground track for satellite FEDSAT.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 1275 DEB LEO 2025-10-23 16:06:05 0.0004440862 451.0 (m) DEBRIS
NOAA 16 DEB SSO 2025-10-18 10:07:31 0.0001126945 254.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-05-30 02:48:44 0.0004511201 182.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2025-04-15 20:55:09 0.0005594599 159.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2025-04-04 06:09:57 0.0001127793 801.0 (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.

FEDSAT 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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