GEESAT 2-06
NORAD 58910
Payload
LEO
2024-023F
● Active
CONNECTING…
LEO · NORAD 58910
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
550 km
Apogee
558 km
Inclination
50.0°
Period
95.7 min
Mean Motion
15.04211795 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude554 km
Orbital Velocity27,313 km/h
Velocity7.59 km/s
Orbital Period96 minutes
Orbits / Day15.04
Eccentricity0.0006
Semi-Major Axis6,925 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2024-02-02
Launch Site
Xichang, China
Int'l Designator
2024-023F
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
GEESAT 2-06 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 550 km and 558 km with an inclination of 50.0°. It travels at approximately 27,313 km/h (7.59 km/s), completing one full orbit every 96 minutes — that’s roughly 15.04 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 554 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 3,395 active payloads and 373 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 19.5% 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 1,219 active satellites in total, of which 152 share a similar altitude band with GEESAT 2-06.
❓ Frequently Asked Questions
GEESAT 2-06 orbits in Low Earth Orbit (LEO) at altitudes between 550 km (perigee) and 558 km (apogee), with an average altitude of approximately 554 km. It completes one orbit every 96 minutes, travelling at approximately 27,313 km/h (16,971 mph).
GEESAT 2-06 is operated by 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, 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 27,313 km/h (16,971 mph) — roughly 7.59 km/s. It completes 15.04 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.