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APSTAR 1A

NORAD 23943 Payload GEO 1996-039A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36003 km
Apogee
36182 km
Inclination
12.7°
Period
1451.8 min
Mean Motion
0.99190781 rev/day
TLE Epoch
2026-06-18 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,093 km
Orbital Velocity11,030 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0021
Semi-Major Axis42,464 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 APT Satellite (China)
Launch Date
1996-07-03
Launch Site
Xichang, China
Int'l Designator
1996-039A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
APSTAR 1A is an active satellite operated by APT Satellite (China), launched on 1996-07-03 from Xichang, China. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,003 km and 36,182 km with an inclination of 12.7°. 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 APSTAR 1A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
APSTAR 1A 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 12.7°, 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 APSTAR 1A’s average altitude, there are currently 160 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 APSTAR 1A.
❓ Frequently Asked Questions
APSTAR 1A orbits at approximately 36,093 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 12.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
APSTAR 1A is operated by APT Satellite (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23943. You can track APSTAR 1A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
APSTAR 1A was launched on 1996-07-03 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks APSTAR 1A (NORAD ID 23943) 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.
APSTAR 1A 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.