ROCSAT 2
NORAD 28254
Payload
LEO
2004-018A
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Altitude (km)
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🛰️ Orbital Parameters
Perigee
888 km
Apogee
891 km
Inclination
98.8°
Period
102.8 min
Mean Motion
14.01261365 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude890 km
Orbital Velocity26,674 km/h
Velocity7.41 km/s
Orbital Period103 minutes
Orbits / Day14.01
Eccentricity0.0002
Semi-Major Axis7,261 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
TWN
Launch Date
2004-05-20
Launch Site
Vandenberg SFB, California
Int'l Designator
2004-018A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ROCSAT 2 is an active satellite operated by TWN, launched on 2004-05-20 from Vandenberg SFB, California. With over 22 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 888 km and 891 km with an inclination of 98.8°. It travels at approximately 26,674 km/h (7.41 km/s), completing one full orbit every 103 minutes — that’s roughly 14.01 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks ROCSAT 2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ROCSAT 2 orbits at an average altitude of 890 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of ROCSAT 2’s average altitude, there are currently 181 active payloads and 1,513 tracked debris or rocket body fragments. With an inclination of 98.8°, ROCSAT 2 passes over latitudes between 98.8°N and 98.8°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. TWN operates approximately 30 active satellites in total.
❓ Frequently Asked Questions
ROCSAT 2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 890 km altitude. Its 98.8° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 103 minutes, travelling at 26,674 km/h.
ROCSAT 2 is operated by TWN. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28254. You can track ROCSAT 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ROCSAT 2 was launched on 2004-05-20 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks ROCSAT 2 (NORAD ID 28254) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
ROCSAT 2 travels at approximately 26,674 km/h (16,574 mph) — roughly 7.41 km/s. It completes 14.01 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.