GEESAT 4-06, 65124
Orbit data source: Space-Track
GEESAT 4-06, 65124 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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65124 intel report (Beta)
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Edit Public Description
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: 5 hours ago
TLE from 5 hours ago
0 GEESAT 4-06
1 65124U 25170F 26035.13139875 .00002935 00000-0 37674-3 0 9995
2 65124 49.9838 71.0177 0019857 254.1787 105.6962 14.83792169 26678Epoch: 2026-02-04T03:09Z
TLE epoch observation values (Epoch: 2026-02-04T03:09:12.852Z)
Latitude
0.00001°
Longitude
-110.58822°
Altitude
621.705 km
Speed
7.547 km/s
True Right ascension
04h 44m 04s
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
10:21:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
632.033 km
Perigee altitude
604.248 km
Semi-major axis
6,996.278 km
Eccentricity
0.00199
Inclination
49.9838°
RAAN
71.0177°
Arg. of periapsis
254.1787°
True anomaly
105.91511°
Mean anomaly
105.6962°
Eccentric anomaly
105.80567°
Mean motion
3.70888 °/min
Orbital period
97.06 mins
BSTAR
0.00037674
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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 4-06 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 | 2026-02-04 10:03:10.085Z | 325.825° NNW | 2026-02-04 10:06:10.085Z | 25.062° NE | 26.79° | 2026-02-04 10:09:10.085Z | 74.324° E |
| 7 mins | 2026-02-04 11:44:10.085Z | 302.204° NW | 2026-02-04 11:47:10.085Z | 283.715° WNW | 43.329° | 2026-02-04 11:51:10.085Z | 129.459° SE |
| 7 mins | 2026-02-05 05:13:10.085Z | 231.036° WSW | 2026-02-05 05:16:10.085Z | 93.039° ESE | 44.643° | 2026-02-05 05:20:10.085Z | 57.015° ENE |
| 6 mins | 2026-02-05 06:55:10.085Z | 293.036° NW | 2026-02-05 06:58:10.085Z | 353.077° N | 26.511° | 2026-02-05 07:01:10.085Z | 40.705° NE |
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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