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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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: 10 hours ago
TLE from 10 hours ago
0 GEESAT 4-05
1 65123U 25170E 26095.89081778 .00002717 00000-0 36743-3 0 9995
2 65123 49.9929 102.7751 0007627 41.3650 318.7863 14.81895205 36328Epoch: 2026-04-05T21:22Z
TLE epoch observation values (Epoch: 2026-04-05T21:22:46.656Z)
Latitude
-0.00008°
Longitude
-52.10911°
Altitude
619.876 km
Speed
7.552 km/s
True Right ascension
06h 51m 06s
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
13:39:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
629.448 km
Perigee altitude
618.767 km
Semi-major axis
7,002.244 km
Eccentricity
0.00076
Inclination
49.9929°
RAAN
102.7751°
Arg. of periapsis
41.365°
True anomaly
318.72867°
Mean anomaly
318.7863°
Eccentric anomaly
318.75749°
Mean motion
3.70414 °/min
Orbital period
97.19 mins
BSTAR
0.00036743
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-04-06 09:10:46.854Z | 312.527° NW | 2026-04-06 09:13:46.854Z | 359.593° N | 39.159° | 2026-04-06 09:17:46.854Z | 106.257° ESE |
| 6 mins | 2026-04-06 10:52:46.854Z | 275.353° WNW | 2026-04-06 10:55:46.854Z | 220.826° SW | 24.842° | 2026-04-06 10:58:46.854Z | 172.548° S |
| 6 mins | 2026-04-07 02:41:46.854Z | 200.509° SSW | 2026-04-07 02:43:46.854Z | 158.169° S | 34.979° | 2026-04-07 02:47:46.854Z | 69.094° E |
| 7 mins | 2026-04-07 04:22:46.854Z | 272.799° WNW | 2026-04-07 04:25:46.854Z | 334.838° NNW | 33.064° | 2026-04-07 04:29:46.854Z | 45.595° ENE |
| 6 mins | 2026-04-07 06:05:46.854Z | 315.545° NNW | 2026-04-07 06:07:46.854Z | 348.084° N | 20.848° | 2026-04-07 06:11:46.854Z | 49.354° ENE |
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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