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: 23 hours ago
TLE from 23 hours ago
0 GEESAT 4-02
1 65120U 25170B 26225.18434152 .00000500 00000-0 86231-4 0 9993
2 65120 49.9856 269.8828 0009914 306.0320 53.9699 14.84197400 54926Epoch: 2026-08-13T04:25Z
TLE epoch observation values (Epoch: 2026-08-13T04:25:27.107Z)
Latitude
-0.00002°
Longitude
-118.10773°
Altitude
612.575 km
Speed
7.556 km/s
True Right ascension
17h 59m 31s
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
17:54:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
623.802 km
Perigee altitude
609.932 km
Semi-major axis
6,995.004 km
Eccentricity
0.00099
Inclination
49.9856°
RAAN
269.8828°
Arg. of periapsis
306.032°
True anomaly
54.06184°
Mean anomaly
53.9699°
Eccentric anomaly
54.01586°
Mean motion
3.70989 °/min
Orbital period
97.04 mins
BSTAR
0.000086231
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-14 04:48:44.896Z | 185.191° SSW | 2026-08-14 04:51:44.896Z | 139.431° SSE | 22.87° | 2026-08-14 04:54:44.896Z | 86.709° E |
| 7 mins | 2026-08-14 06:29:44.896Z | 251.201° W | 2026-08-14 06:32:44.896Z | 303.6° NW | 40.896° | 2026-08-14 06:36:44.896Z | 49.174° ENE |
| 6 mins | 2026-08-14 08:12:44.896Z | 306.669° NW | 2026-08-14 08:14:44.896Z | 341.5° N | 22.847° | 2026-08-14 08:18:44.896Z | 44.808° NE |
| 5 mins | 2026-08-14 09:55:44.896Z | 335.816° NNW | 2026-08-14 09:57:44.896Z | 15.201° NNE | 22.985° | 2026-08-14 10:00:44.896Z | 62.294° ENE |
| 7 mins | 2026-08-14 11:36:44.896Z | 314.512° NW | 2026-08-14 11:39:44.896Z | 45.441° ENE | 41.304° | 2026-08-14 11:43:44.896Z | 111.104° ESE |
| 5 mins | 2026-08-14 13:18:44.896Z | 263.002° W | 2026-08-14 13:20:44.896Z | 224.129° SW | 23.338° | 2026-08-14 13:23:44.896Z | 176.043° S |
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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