FEDSAT

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite FEDSAT 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 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: 100.731 minutes

Inclination: 98.8052 deg

SMA: 7171.354 km

Apoapsis: 800.481 km

Periapsis: 785.958 km

RAAN: 87.6208 deg

Eccentricy: 0.0010126

Argument of periapsis: 88.4542 deg

Mean anomaly: 271.7799 deg

Mean motion: 14.29555369 rev/day

Mean motion (dot): 0.00000252 rev/day2

B* drag term: 0.00011633 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, 8:46 p.m. UTC

TLE line 0: 0 FEDSAT

TLE line 1: 1 27598U 02056B 25124.86580250 .00000252 00000-0 11633-3 0 9998

TLE line 2: 2 27598 98.8052 87.6208 0010126 88.4542 271.7799 14.29555369167417

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 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
COSMOS 1867 COOLANT LEO 2025-02-01 11:31:37 0.0003421807 126.0 (m) DEBRIS
NOAA 16 DEB SSO 2025-01-18 16:48:28 0.000113056 58.0 (m) DEBRIS
DELTA 1 DEB SSO 2024-12-16 18:25:52 0.0001288985 490.0 (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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