Key statistics
Satellite ROCSAT 2 at a glance.
Uptime
7719
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: 98.7967 deg
SMA: 7267.745 km
Apoapsis: 889.955 km
Periapsis: 889.264 km
RAAN: 162.9864 deg
Eccentricy: 0.0000476
Argument of periapsis: 150.9278 deg
Mean anomaly: 268.461 deg
Mean motion: 14.01210181 rev/day
Mean motion (dot): 0.00000301 rev/day2
B* drag term: 0.00022828 1/REarth
Two-line elements (TLE)
Creation date: July 8, 2025, 2:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 7, 2025, 10:23 p.m. UTC
TLE line 0: 0 ROCSAT 2
TLE line 1: 1 28254U 04018A 25188.93297693 .00000301 00000-0 22828-3 0 9995
TLE line 2: 2 28254 98.7967 162.9864 0000476 150.9278 268.4610 14.01210181 80547
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.
Go to all conjunctionsAssociated 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.
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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