GEESAT 2-04
NORAD 58908
Payload
LEO
2024-023D
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LEO · NORAD 58908
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
571 km
Apogee
580 km
Inclination
50.0°
Period
96.2 min
Mean Motion
14.97196160 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude576 km
Orbital Velocity27,270 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day14.97
Eccentricity0.0006
Semi-Major Axis6,947 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2024-02-02
Launch Site
Xichang, China
Int'l Designator
2024-023D
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
GEESAT 2-04 is an active satellite operated by China, launched on 2024-02-02 from Xichang, China. It orbits in Low Earth Orbit (LEO) at altitudes between 571 km and 580 km with an inclination of 50.0°. It travels at approximately 27,270 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 14.97 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks GEESAT 2-04 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GEESAT 2-04 orbits at an average altitude of 576 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of GEESAT 2-04’s average altitude, there are currently 3,104 active payloads and 515 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-2112, STARLINK-2722. This makes it one of the more crowded altitude bands, containing roughly 17.8% of all active satellites. With an inclination of 50.0°, GEESAT 2-04 passes over latitudes between 50.0°N and 50.0°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 1,218 active satellites in total, of which 178 share a similar altitude band with GEESAT 2-04.
❓ Frequently Asked Questions
GEESAT 2-04 orbits in Low Earth Orbit (LEO) at altitudes between 571 km (perigee) and 580 km (apogee), with an average altitude of approximately 576 km. It completes one orbit every 96 minutes, travelling at approximately 27,270 km/h (16,945 mph).
GEESAT 2-04 is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 58908. You can track GEESAT 2-04 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GEESAT 2-04 was launched on 2024-02-02 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks GEESAT 2-04 (NORAD ID 58908) 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.
GEESAT 2-04 travels at approximately 27,270 km/h (16,945 mph) — roughly 7.58 km/s. It completes 14.97 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.