DOUBLESTAR (TC-2)
NORAD 28382
Payload
MEO
2004-029A
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
416 km
Apogee
31252 km
Inclination
87.9°
Period
549.1 min
Mean Motion
2.62252050 rev/day
TLE Epoch
2026-09-17 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude15,834 km
Orbital Velocity15,253 km/h
Velocity4.24 km/s
Orbital Period9 hours 9 minutes
Orbits / Day2.62
Eccentricity0.6943
Semi-Major Axis22,205 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 CASC (China)
Launch Date
2004-07-25
Launch Site
Taiyuan Satellite Launch Center, China
Int'l Designator
2004-029A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
DOUBLESTAR (TC-2) is an active satellite operated by CASC (China), launched on 2004-07-25 from Taiyuan Satellite Launch Center, China on the Double Star DSP-P launch. With over 22 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 416 km and 31,252 km with an inclination of 87.9°. It travels at approximately 15,253 km/h (4.24 km/s), completing one full orbit every 9 hours 9 minutes — that’s roughly 2.62 orbits per day. Its orbital eccentricity of 0.6943 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks DOUBLESTAR (TC-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
DOUBLESTAR (TC-2) orbits at an average altitude of 15,834 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of DOUBLESTAR (TC-2)’s average altitude, there are currently 2 active payloads and 7 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 87.9°, DOUBLESTAR (TC-2) passes over latitudes between 87.9°N and 87.9°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. China operates approximately 1,275 active satellites in total.
❓ Frequently Asked Questions
DOUBLESTAR (TC-2) orbits in Medium Earth Orbit (MEO) at altitudes between 416 km (perigee) and 31,252 km (apogee), with an average altitude of approximately 15,834 km. It completes one orbit every 9 hours 9 minutes, travelling at approximately 15,253 km/h (9,478 mph).
DOUBLESTAR (TC-2) is operated by CASC (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28382. You can track DOUBLESTAR (TC-2) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DOUBLESTAR (TC-2) was launched on 2004-07-25 from Taiyuan Satellite Launch Center, China. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks DOUBLESTAR (TC-2) (NORAD ID 28382) 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.
DOUBLESTAR (TC-2) travels at approximately 15,253 km/h (9,478 mph) — roughly 4.24 km/s. It completes 2.62 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.