Skip to content
Home Library Satellite Directory CHINASAT 5B (SINOSAT 1)

CHINASAT 5B (SINOSAT 1)

NORAD 25404 Payload GEO 1998-044A ● Active
CONNECTING… GEO · NORAD 25404
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
36076 km
Apogee
36107 km
Inclination
11.0°
Period
1451.7 min
Mean Motion
0.99195853 rev/day
TLE Epoch
2026-06-18 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,092 km
Orbital Velocity11,030 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0004
Semi-Major Axis42,463 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China Satellite Communications (China)
Launch Date
1998-07-18
Launch Site
Xichang, China
Int'l Designator
1998-044A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
CHINASAT 5B (SINOSAT 1) is an active satellite operated by China Satellite Communications (China), launched on 1998-07-18 from Xichang, China. With over 28 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,076 km and 36,107 km with an inclination of 11.0°. It travels at approximately 11,030 km/h (3.06 km/s), completing one full orbit every 24.2 hours — that’s roughly 0.99 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 CHINASAT 5B (SINOSAT 1) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CHINASAT 5B (SINOSAT 1) 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 11.0°, 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. Within ±50 km of CHINASAT 5B (SINOSAT 1)’s average altitude, there are currently 159 active payloads and 10 tracked debris or rocket body fragments. China operates approximately 1,219 active satellites in total, of which 11 share a similar altitude band with CHINASAT 5B (SINOSAT 1).
❓ Frequently Asked Questions
CHINASAT 5B (SINOSAT 1) orbits at approximately 36,092 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 11,030 km/h — it just keeps pace with the ground below. With an inclination of 11.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
CHINASAT 5B (SINOSAT 1) is operated by China Satellite Communications (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25404. You can track CHINASAT 5B (SINOSAT 1) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CHINASAT 5B (SINOSAT 1) was launched on 1998-07-18 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks CHINASAT 5B (SINOSAT 1) (NORAD ID 25404) 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.
CHINASAT 5B (SINOSAT 1) travels at approximately 11,030 km/h (6,854 mph) — roughly 3.06 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.