ROCSAT 2

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite ROCSAT 2 at a glance.

Uptime

7828

Days in orbit

Revolutions

≈ 14.0

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.8

Latest

Satellite identification and parameters

Extended collection of information and parameters for ROCSAT 2.

Object identification

Identified? True

Debris? False

Object name: ROCSAT 2

International designator: 2004-018A

Object number (NORAD): 28254

Object ID (CCSDS): 28254

Country: TAIWAN (TWN)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 102.768 minutes

Inclination: 98.8127 deg

SMA: 7267.728 km

Apoapsis: 889.918 km

Periapsis: 889.268 km

RAAN: 268.1108 deg

Eccentricy: 0.0000447

Argument of periapsis: 233.6566 deg

Mean anomaly: 180.5767 deg

Mean motion: 14.01214937 rev/day

Mean motion (dot): -0.00000196 rev/day2

B* drag term: -0.00010215674 1/REarth

Two-line elements (TLE)

Creation date: Oct. 25, 2025, 3:11 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 24, 2025, 9:31 p.m. UTC

TLE line 0: 0 ROCSAT 2

TLE line 1: 1 28254U 04018A 25297.89709605 -.00000196 00000-0 -10216-3 0 9994

TLE line 2: 2 28254 98.8127 268.1108 0000447 233.6566 180.5767 14.01214937 95808

Live tracking on map

Real-time ground track for satellite ROCSAT 2.

In-orbit conjunctions

There are no conjunctions computed for ROCSAT 2, at the moment. Check back to stay up to date, as we update our databases every day.

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Associated space launch

ROCSAT 2 (Republic of China Satellite 2) is the second high-resolution Earth observation satellite for the Taiwanese National Space Program Office (NSPO) whose mission is regional remote sensing – to collect data to be used for natural disaster evaluation, agricultural applications, urban planning strategy, environmental monitoring, and ocean surveillance. In addition, the satellite's payload will include an auroral observation instrument.

ROCSAT 2 was lifted into orbit during the mission ‘Taurus 3210 | Formosat-2’, on board a Minotaur-C 3210 space rocket.

The launch took place on May 20, 2004, 5:47 p.m. from Space Launch Complex 576E.

For more information about the launch, click the button.

Launch to space Taurus 3210 | Formosat-2
Taurus 3210 | Formosat-2

Agency: N/A

Status: Launch Successful

Launch date: May 20, 2004, 5:47 p.m. UTC

Rocket: Minotaur-C 3210

Launch pad: Space Launch Complex 576E

Location: Vandenberg SFB, CA, USA

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Latest news about this satellite

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