GEESAT 4-06, 65124
Orbit data source: Space-Track
GEESAT 4-06, 65124 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Fri, 08 Aug 2025 UTC via a JIELONG-3 launch vehicle from the Yellow Sea Launch Area, China (YSLA). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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65124 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GWCG
Mission
Operational Commercial Navigation
Bus & Motor
GPS100, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 GEESAT 4-06
1 65124U 25170F 26289.26637892 .00001397 00000-0 19145-3 0 9996
2 65124 49.9854 332.3499 0018324 147.5283 212.6787 14.84344484 64412Epoch: 2026-10-16T06:23Z
TLE epoch observation values (Epoch: 2026-10-16T06:23:35.138Z)
Latitude
0.00001°
Longitude
-148.33636°
Altitude
626.98 km
Speed
7.541 km/s
True Right ascension
22h 09m 23s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
09:10:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
629.222 km
Perigee altitude
603.588 km
Semi-major axis
6,994.542 km
Eccentricity
0.00183
Inclination
49.9854°
RAAN
332.3499°
Arg. of periapsis
147.5283°
True anomaly
212.56555°
Mean anomaly
212.6787°
Eccentric anomaly
212.6221°
Mean motion
3.71026 °/min
Orbital period
97.03 mins
BSTAR
0.00019145
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Other satellites on launch #170 in the year 2025 (2025-08-08 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GEESAT 4-06 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-10-17 05:10:03.475Z | 202.751° SW | 2026-10-17 05:14:03.475Z | 132.646° SE | 37.828° | 2026-10-17 05:18:03.475Z | 69.44° E |
| 7 mins | 2026-10-17 06:52:03.475Z | 265.717° W | 2026-10-17 06:55:03.475Z | 326.476° NNW | 45.908° | 2026-10-17 06:59:03.475Z | 45.821° ENE |
| 5 mins | 2026-10-17 08:35:03.475Z | 313.897° NW | 2026-10-17 08:37:03.475Z | 347.518° N | 22.767° | 2026-10-17 08:40:03.475Z | 38.549° NE |
| 6 mins | 2026-10-17 10:17:03.475Z | 325.607° NNW | 2026-10-17 10:20:03.475Z | 22.325° NNE | 27.556° | 2026-10-17 10:23:03.475Z | 70.543° E |
| 6 mins | 2026-10-17 11:59:03.475Z | 306.561° NW | 2026-10-17 12:02:03.475Z | 110.686° ESE | 69.834° | 2026-10-17 12:05:03.475Z | 122.848° SE |
| 4 mins | 2026-10-17 13:41:03.475Z | 251.482° W | 2026-10-17 13:42:03.475Z | 235.729° WSW | 16.586° | 2026-10-17 13:45:03.475Z | 191.901° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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