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APSTAR 6E SPS

NORAD 55447 Payload MEO 2023-005C ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
2063 km
Apogee
7025 km
Inclination
28.7°
Period
189.3 min
Mean Motion
7.60562948 rev/day
TLE Epoch
2026-06-18 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude4,544 km
Orbital Velocity21,755 km/h
Velocity6.04 km/s
Orbital Period3 hours 9 minutes
Orbits / Day7.61
Eccentricity0.2273
Semi-Major Axis10,915 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 APT Satellite (China)
Launch Date
2023-01-12
Launch Site
Xichang, China
Int'l Designator
2023-005C
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
APSTAR 6E SPS is an active satellite operated by APT Satellite (China), launched on 2023-01-12 from Xichang, China. It orbits in Medium Earth Orbit (MEO) at altitudes between 2,063 km and 7,025 km with an inclination of 28.7°. It travels at approximately 21,755 km/h (6.04 km/s), completing one full orbit every 3 hours 9 minutes — that’s roughly 7.61 orbits per day. Its orbital eccentricity of 0.2273 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks APSTAR 6E SPS 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 6E SPS orbits at an average altitude of 4,544 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 APSTAR 6E SPS’s average altitude, there are currently 1 active payload and 2 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 28.7°, APSTAR 6E SPS passes over latitudes between 28.7°N and 28.7°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. China operates approximately 1,219 active satellites in total.
❓ Frequently Asked Questions
APSTAR 6E SPS orbits in Medium Earth Orbit (MEO) at altitudes between 2,063 km (perigee) and 7,025 km (apogee), with an average altitude of approximately 4,544 km. It completes one orbit every 3 hours 9 minutes, travelling at approximately 21,755 km/h (13,518 mph).
APSTAR 6E SPS is operated by APT Satellite (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 55447. You can track APSTAR 6E SPS in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
APSTAR 6E SPS was launched on 2023-01-12 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks APSTAR 6E SPS (NORAD ID 55447) 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 6E SPS travels at approximately 21,755 km/h (13,518 mph) — roughly 6.04 km/s. It completes 7.61 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 15 sunrises and sunsets every 24 hours.