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GEESAT 4-05

NORAD 65123 Payload LEO 2025-170E ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
617 km
Apogee
628 km
Inclination
50.0°
Period
97.2 min
Mean Motion
14.82146482 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude623 km
Orbital Velocity27,178 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.82
Eccentricity0.0008
Semi-Major Axis6,994 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-08-08
Launch Site
YSLA
Int'l Designator
2025-170E
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GEESAT 4-05 is an active satellite operated by China, launched on 2025-08-08 from YSLA. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 617 km and 628 km with an inclination of 50.0°. It travels at approximately 27,178 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.82 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 ~10–25 years. Orbital Radar tracks GEESAT 4-05 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 4-05 orbits at an average altitude of 623 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of GEESAT 4-05’s average altitude, there are currently 833 active payloads and 789 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3055, STARLINK-3109. With an inclination of 50.0°, GEESAT 4-05 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 132 share a similar altitude band with GEESAT 4-05.
❓ Frequently Asked Questions
GEESAT 4-05 orbits in Low Earth Orbit (LEO) at altitudes between 617 km (perigee) and 628 km (apogee), with an average altitude of approximately 623 km. It completes one orbit every 97 minutes, travelling at approximately 27,178 km/h (16,888 mph).
GEESAT 4-05 is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 65123. You can track GEESAT 4-05 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GEESAT 4-05 was launched on 2025-08-08 from YSLA. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks GEESAT 4-05 (NORAD ID 65123) 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 4-05 travels at approximately 27,178 km/h (16,888 mph) — roughly 7.55 km/s. It completes 14.82 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.