GEESAT 4-05, 65123
Orbit data source: Space-Track
GEESAT 4-05, 65123 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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65123 intel report (Beta)
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Edit Public Description
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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 GEESAT 4-05
1 65123U 25170E 26034.55336554 .00047872 00000-0 10437-2 0 9998
2 65123 49.9968 42.1369 0023950 338.6836 21.3127 15.43421841 27014Epoch: 2026-02-03T13:16Z
TLE epoch observation values (Epoch: 2026-02-03T13:16:50.782Z)
Latitude
-0.00008°
Longitude
69.19259°
Altitude
421.38 km
Speed
7.668 km/s
True Right ascension
02h 48m 32s
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
08:37:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.12 km
Perigee altitude
420.476 km
Semi-major axis
6,814.935 km
Eccentricity
0.0024
Inclination
49.9968°
RAAN
42.1369°
Arg. of periapsis
338.6836°
True anomaly
21.41273°
Mean anomaly
21.3127°
Eccentric anomaly
21.36269°
Mean motion
3.8579 °/min
Orbital period
93.32 mins
BSTAR
0.0010437
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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 4-05 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-04 08:22:26.121Z | 335.266° NNW | 2026-02-04 08:24:26.121Z | 28.828° NE | 25.138° | 2026-02-04 08:26:26.121Z | 74.484° E |
| 5 mins | 2026-02-04 09:59:26.121Z | 289.573° WNW | 2026-02-04 10:01:26.121Z | 237.248° WSW | 37.482° | 2026-02-04 10:04:26.121Z | 145.451° SSE |
| 4 mins | 2026-02-05 02:46:26.121Z | 201.743° SSW | 2026-02-05 02:47:26.121Z | 167.99° S | 36.289° | 2026-02-05 02:50:26.121Z | 67.863° E |
| 4 mins | 2026-02-05 04:23:26.121Z | 290.752° WNW | 2026-02-05 04:25:26.121Z | 343.402° N | 24.65° | 2026-02-05 04:27:26.121Z | 30.186° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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