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SINOSAT 2

NORAD 29516 Payload GEO 2006-048A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
37835 km
Apogee
38154 km
Inclination
14.4°
Period
1550.4 min
Mean Motion
0.92881940 rev/day
TLE Epoch
2026-06-18 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude37,995 km
Orbital Velocity10,791 km/h
Velocity3.00 km/s
Orbital Period25.8 hours
Orbits / Day0.93
Eccentricity0.0036
Semi-Major Axis44,366 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2006-10-28
Launch Site
Xichang, China
Int'l Designator
2006-048A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SINOSAT 2 is an active satellite operated by China, launched on 2006-10-28 from Xichang, China. With over 20 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 37,835 km and 38,154 km with an inclination of 14.4°. It travels at approximately 10,791 km/h (3.00 km/s), completing one full orbit every 25.8 hours — that’s roughly 0.93 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks SINOSAT 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
SINOSAT 2 occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 14.4°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. China operates approximately 1,219 active satellites in total.
❓ Frequently Asked Questions
SINOSAT 2 orbits at approximately 37,995 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 10,791 km/h — it just keeps pace with the ground below. With an inclination of 14.4°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
SINOSAT 2 is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 29516. You can track SINOSAT 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SINOSAT 2 was launched on 2006-10-28 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks SINOSAT 2 (NORAD ID 29516) 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.
SINOSAT 2 travels at approximately 10,791 km/h (6,705 mph) — roughly 3.00 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.