GEESAT 2-06
NORAD 58910
Payload
LEO
2024-023F
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LEO · NORAD 58910
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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
548 km
Apogee
556 km
Inclination
50.0°
Period
95.7 min
Mean Motion
15.04900417 rev/day
TLE Epoch
2026-09-17 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude552 km
Orbital Velocity27,316 km/h
Velocity7.59 km/s
Orbital Period96 minutes
Orbits / Day15.05
Eccentricity0.0006
Semi-Major Axis6,923 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Geespace (China)
Launch Date
2024-02-02
Launch Site
Xichang Satellite Launch Center, China
Int'l Designator
2024-023F
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
GEESAT 2-06 is an active satellite operated by Geespace (China), launched on 2024-02-02 from Xichang Satellite Launch Center, China on the GeeSat launch. It orbits in Low Earth Orbit (LEO) at altitudes between 548 km and 556 km with an inclination of 50.0°. It travels at approximately 27,316 km/h (7.59 km/s), completing one full orbit every 96 minutes — that’s roughly 15.05 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 2-06 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 2-06 orbits at an average altitude of 552 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 2-06’s average altitude, there are currently 1,688 active payloads and 407 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 9% of all active satellites. With an inclination of 50.0°, GEESAT 2-06 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 1,275 active satellites in total, of which 148 share a similar altitude band with GEESAT 2-06.
❓ Frequently Asked Questions
GEESAT 2-06 orbits in Low Earth Orbit (LEO) at altitudes between 548 km (perigee) and 556 km (apogee), with an average altitude of approximately 552 km. It completes one orbit every 96 minutes, travelling at approximately 27,316 km/h (16,974 mph).
GEESAT 2-06 is operated by Geespace (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 58910. You can track GEESAT 2-06 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GEESAT 2-06 was launched on 2024-02-02 from Xichang Satellite Launch Center, 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 2-06 (NORAD ID 58910) 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 2-06 travels at approximately 27,316 km/h (16,974 mph) — roughly 7.59 km/s. It completes 15.05 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.