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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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Taizhou Xingkong
Mission
Operational spacecraft
Bus & Motor
GEESAT1, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.9 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 GEESAT 4-04
1 65122U 25170D 25283.38832470 .00003741 00000-0 44201-3 0 9995
2 65122 49.9815 252.6943 0010135 192.7280 167.3405 14.86680378 9336Epoch: 2025-10-10T09:19Z
TLE epoch observation values (Epoch: 2025-10-10T09:19:11.254Z)
Latitude
0.00001°
Longitude
93.66254°
Altitude
615.768 km
Speed
7.549 km/s
True Right ascension
16h 50m 46s
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
19:05:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
616.16 km
Perigee altitude
601.997 km
Semi-major axis
6,987.216 km
Eccentricity
0.00101
Inclination
49.9815°
RAAN
252.6943°
Arg. of periapsis
192.728°
True anomaly
167.36592°
Mean anomaly
167.3405°
Eccentric anomaly
167.35321°
Mean motion
3.7161 °/min
Orbital period
96.88 mins
BSTAR
0.00044201
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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 | 2025-10-11 01:39:47.231Z | 250.155° W | 2025-10-11 01:43:47.231Z | 348.658° N | 41.081° | 2025-10-11 01:47:47.231Z | 50.857° ENE |
| 6 mins | 2025-10-11 03:22:47.231Z | 304.133° NW | 2025-10-11 03:25:47.231Z | 358.784° N | 22.467° | 2025-10-11 03:28:47.231Z | 43.171° NE |
| 5 mins | 2025-10-11 05:05:47.231Z | 335.293° NNW | 2025-10-11 05:07:47.231Z | 14.614° NNE | 22.641° | 2025-10-11 05:10:47.231Z | 62.197° ENE |
| 7 mins | 2025-10-11 06:46:47.231Z | 315.329° NNW | 2025-10-11 06:49:47.231Z | 56.413° ENE | 40.626° | 2025-10-11 06:53:47.231Z | 111.55° ESE |
| 6 mins | 2025-10-11 08:27:47.231Z | 271.562° WNW | 2025-10-11 08:30:47.231Z | 216.371° SW | 22.516° | 2025-10-11 08:33:47.231Z | 172.837° S |
| 7 mins | 2025-10-12 00:12:47.231Z | 205.838° SW | 2025-10-12 00:15:47.231Z | 139.621° SSE | 36.205° | 2025-10-12 00:19:47.231Z | 66.689° ENE |
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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