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, 0.9 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 GEESAT 4-06
1 65124U 25170F 26225.91342261 .00000543 00000-0 91437-4 0 9998
2 65124 49.9840 266.3157 0019134 262.8123 97.0640 14.84195097 55000Epoch: 2026-08-13T21:55Z
TLE epoch observation values (Epoch: 2026-08-13T21:55:19.713Z)
Latitude
-0.00002°
Longitude
-24.86264°
Altitude
618.327 km
Speed
7.55 km/s
True Right ascension
17h 45m 15s
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
18:55:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.259 km
Perigee altitude
603.49 km
Semi-major axis
6,995.012 km
Eccentricity
0.00191
Inclination
49.984°
RAAN
266.3157°
Arg. of periapsis
262.8123°
True anomaly
97.28153°
Mean anomaly
97.064°
Eccentric anomaly
97.17277°
Mean motion
3.70989 °/min
Orbital period
97.04 mins
BSTAR
0.000091437
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-14 04:32:30.168Z | 167.295° S | 2026-08-14 04:34:30.168Z | 137.421° SSE | 17.97° | 2026-08-14 04:37:30.168Z | 91.598° ESE |
| 7 mins | 2026-08-14 06:12:30.168Z | 240.847° WSW | 2026-08-14 06:15:30.168Z | 278.829° WNW | 43.922° | 2026-08-14 06:19:30.168Z | 53.276° ENE |
| 6 mins | 2026-08-14 07:55:30.168Z | 303.512° NW | 2026-08-14 07:57:30.168Z | 341.659° N | 24.904° | 2026-08-14 08:01:30.168Z | 44.631° NE |
| 6 mins | 2026-08-14 09:37:30.168Z | 322.963° NNW | 2026-08-14 09:40:30.168Z | 15.161° NNE | 21.913° | 2026-08-14 09:43:30.168Z | 58.98° ENE |
| 7 mins | 2026-08-14 11:19:30.168Z | 319.509° NNW | 2026-08-14 11:22:30.168Z | 39.317° NE | 37.359° | 2026-08-14 11:26:30.168Z | 102.965° ESE |
| 7 mins | 2026-08-14 13:00:30.168Z | 281.103° WNW | 2026-08-14 13:03:30.168Z | 224.32° SW | 29.238° | 2026-08-14 13:07:30.168Z | 160.246° S |
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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