GEESAT 4-08, 65126
Orbit data source: Space-Track
GEESAT 4-08, 65126 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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65126 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, 1.0 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 GEESAT 4-08
1 65126U 25170H 26095.91420826 .00002839 00000-0 37529-3 0 9990
2 65126 49.9650 101.7344 0021024 55.1092 305.1818 14.82640630 36331Epoch: 2026-04-05T21:56Z
TLE epoch observation values (Epoch: 2026-04-05T21:56:27.593Z)
Latitude
-0.00001°
Longitude
-61.59338°
Altitude
613.084 km
Speed
7.558 km/s
True Right ascension
06h 46m 56s
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
11:42:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
636.482 km
Perigee altitude
607.048 km
Semi-major axis
6,999.902 km
Eccentricity
0.0021
Inclination
49.965°
RAAN
101.7344°
Arg. of periapsis
55.1092°
True anomaly
304.98459°
Mean anomaly
305.1818°
Eccentric anomaly
305.08323°
Mean motion
3.706 °/min
Orbital period
97.14 mins
BSTAR
0.00037529
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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 4-08 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 | 2026-04-06 06:22:24.444Z | 313.657° NW | 2026-04-06 06:25:24.444Z | 5.742° NNE | 20.596° | 2026-04-06 06:28:24.444Z | 48.287° ENE |
| 5 mins | 2026-04-06 08:05:24.444Z | 334.227° NNW | 2026-04-06 08:07:24.444Z | 17.244° NNE | 26.735° | 2026-04-06 08:10:24.444Z | 72.251° E |
| 7 mins | 2026-04-06 09:46:24.444Z | 300.897° NW | 2026-04-06 09:49:24.444Z | 179.606° S | 44.393° | 2026-04-06 09:53:24.444Z | 129.898° SE |
| 7 mins | 2026-04-07 03:15:24.444Z | 232.932° WSW | 2026-04-07 03:18:24.444Z | 210.038° SW | 44.757° | 2026-04-07 03:22:24.444Z | 56.563° ENE |
| 5 mins | 2026-04-07 04:58:24.444Z | 301.228° NW | 2026-04-07 05:00:24.444Z | 343.112° N | 25.831° | 2026-04-07 05:03:24.444Z | 37.399° 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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