GEESAT 4-02, 65120
Orbit data source: Space-Track
GEESAT 4-02, 65120 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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65120 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, 14.5 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 GEESAT 4-02
1 65120U 25170B 26095.62775963 .00002848 00000-0 36531-3 0 9999
2 65120 49.9836 150.7631 0009484 169.8973 190.2157 14.83994668 35681Epoch: 2026-04-05T15:03Z
TLE epoch observation values (Epoch: 2026-04-05T15:03:58.432Z)
Latitude
-0.00003°
Longitude
90.83914°
Altitude
623.814 km
Speed
7.545 km/s
True Right ascension
10h 03m 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
11:45:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
624.139 km
Perigee altitude
610.87 km
Semi-major axis
6,995.641 km
Eccentricity
0.00095
Inclination
49.9836°
RAAN
150.7631°
Arg. of periapsis
169.8973°
True anomaly
190.19645°
Mean anomaly
190.2157°
Eccentric anomaly
190.20607°
Mean motion
3.70938 °/min
Orbital period
97.05 mins
BSTAR
0.00036531
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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 4-02 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 | 2026-04-06 05:47:52.144Z | 173.45° S | 2026-04-06 05:49:52.144Z | 124.933° SE | 27.631° | 2026-04-06 05:52:52.144Z | 76.778° E |
| 7 mins | 2026-04-06 07:27:52.144Z | 262.396° W | 2026-04-06 07:30:52.144Z | 340.17° N | 38.145° | 2026-04-06 07:34:52.144Z | 48.593° ENE |
| 5 mins | 2026-04-06 09:10:52.144Z | 316.034° NNW | 2026-04-06 09:12:52.144Z | 353.035° N | 21.945° | 2026-04-06 09:15:52.144Z | 41.207° NE |
| 6 mins | 2026-04-06 10:52:52.144Z | 328.635° NNW | 2026-04-06 10:54:52.144Z | 4.362° NNE | 23.92° | 2026-04-06 10:58:52.144Z | 70.255° E |
| 7 mins | 2026-04-06 12:33:52.144Z | 308.272° NW | 2026-04-06 12:36:52.144Z | 353.899° N | 43.542° | 2026-04-06 12:40:52.144Z | 117.881° SE |
| 4 mins | 2026-04-06 14:16:52.144Z | 250.594° W | 2026-04-06 14:17:52.144Z | 233.168° WSW | 18.546° | 2026-04-06 14:20:52.144Z | 186.792° SSW |
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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