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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 GEESAT 4-04
1 65122U 25170D 26095.93346034 .00003012 00000-0 39327-3 0 9998
2 65122 49.9690 102.0162 0026282 30.0988 330.1453 14.82911193 36338Epoch: 2026-04-05T22:24Z
TLE epoch observation values (Epoch: 2026-04-05T22:24:10.973Z)
Latitude
-0.00007°
Longitude
-68.26135°
Altitude
604.751 km
Speed
7.567 km/s
True Right ascension
06h 48m 03s
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
13:39:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
639.308 km
Perigee altitude
602.518 km
Semi-major axis
6,999.05 km
Eccentricity
0.00263
Inclination
49.969°
RAAN
102.0162°
Arg. of periapsis
30.0988°
True anomaly
329.99495°
Mean anomaly
330.1453°
Eccentric anomaly
330.07017°
Mean motion
3.70668 °/min
Orbital period
97.12 mins
BSTAR
0.00039327
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-06 08:32:23.796Z | 314.525° NW | 2026-04-06 08:36:23.796Z | 23.272° NE | 31.883° | 2026-04-06 08:40:23.796Z | 91.111° ESE |
| 6 mins | 2026-04-06 10:15:23.796Z | 286.526° WNW | 2026-04-06 10:18:23.796Z | 198.392° SSW | 36.961° | 2026-04-06 10:21:23.796Z | 148.765° SSE |
| 5 mins | 2026-04-07 02:04:23.796Z | 164.812° S | 2026-04-07 02:06:23.796Z | 124.679° SE | 21.929° | 2026-04-07 02:09:23.796Z | 80.697° E |
| 7 mins | 2026-04-07 03:44:23.796Z | 253.085° W | 2026-04-07 03:47:23.796Z | 349.502° N | 41.363° | 2026-04-07 03:51:23.796Z | 51.189° ENE |
| 5 mins | 2026-04-07 05:27:23.796Z | 313.802° NW | 2026-04-07 05:29:23.796Z | 353.46° N | 22.723° | 2026-04-07 05:32:23.796Z | 41.06° NE |
| 6 mins | 2026-04-07 07:09:23.796Z | 328.372° NNW | 2026-04-07 07:11:23.796Z | 3.674° NNE | 22.572° | 2026-04-07 07:15:23.796Z | 66.206° ENE |
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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