GEESAT 4-04, 65122
Orbit data source: Space-Track
GEESAT 4-04, 65122 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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65122 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: 23 hours ago
TLE from 23 hours ago
0 GEESAT 4-04
1 65122U 25170D 26225.17457242 .00000489 00000-0 88586-4 0 9990
2 65122 49.9692 224.0851 0029478 172.5850 187.5529 14.82301179 55505Epoch: 2026-08-13T04:11Z
TLE epoch observation values (Epoch: 2026-08-13T04:11:23.057Z)
Latitude
0.00001°
Longitude
-160.3789°
Altitude
643.066 km
Speed
7.527 km/s
True Right ascension
14h 56m 20s
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
17:53:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
643.47 km
Perigee altitude
602.195 km
Semi-major axis
7,000.97 km
Eccentricity
0.00295
Inclination
49.9692°
RAAN
224.0851°
Arg. of periapsis
172.585°
True anomaly
187.50866°
Mean anomaly
187.5529°
Eccentric anomaly
187.53076°
Mean motion
3.70515 °/min
Orbital period
97.16 mins
BSTAR
0.000088586
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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 4-04 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 | 2026-08-14 04:44:09.169Z | 285.694° WNW | 2026-08-14 04:48:09.169Z | 355.267° N | 25.76° | 2026-08-14 04:51:09.169Z | 41.467° NE |
| 5 mins | 2026-08-14 06:28:09.169Z | 328.019° NNW | 2026-08-14 06:30:09.169Z | 3.516° NNE | 21.409° | 2026-08-14 06:33:09.169Z | 52.137° ENE |
| 6 mins | 2026-08-14 08:10:09.169Z | 324.982° NNW | 2026-08-14 08:12:09.169Z | 9.853° NNE | 34.398° | 2026-08-14 08:16:09.169Z | 95.364° ESE |
| 6 mins | 2026-08-14 09:51:09.169Z | 283.218° WNW | 2026-08-14 09:54:09.169Z | 216.912° SW | 32.353° | 2026-08-14 09:57:09.169Z | 159.549° S |
| 6 mins | 2026-08-15 01:40:09.169Z | 181.566° SSW | 2026-08-15 01:42:09.169Z | 140.97° SSE | 27.942° | 2026-08-15 01:46:09.169Z | 74.328° E |
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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