GJZ 01, 62290
Orbit data source: Space-Track
GJZ 01, 62290 is a payload satellite owned by CASC (CN) in LEO that was launched on Thu, 12 Dec 2024 UTC via a CHANG ZHENG 2D/YZ-3 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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62290 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
HITSAT
Mission
Operational Civil Communications
Bus & Motor
HARBFLAT, Unknown motor
Mass
~150 kg wet, ~150 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.5 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 GJZ 01
1 62290U 24238A 25258.66218087 -.00000098 00000-0 22276-4 0 9999
2 62290 59.9141 37.5824 0026724 55.1376 305.2139 13.75157671 37845Epoch: 2025-09-15T15:53Z
TLE epoch observation values (Epoch: 2025-09-15T15:53:32.427Z)
Latitude
-0.00001°
Longitude
164.33366°
Altitude
971.291 km
Speed
7.372 km/s
True Right ascension
02h 30m 19s
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
19:08:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,000.045 km
Perigee altitude
960.715 km
Semi-major axis
7,358.517 km
Eccentricity
0.00267
Inclination
59.9141°
RAAN
37.5824°
Arg. of periapsis
55.1376°
True anomaly
304.96322°
Mean anomaly
305.2139°
Eccentric anomaly
305.08861°
Mean motion
3.43841 °/min
Orbital period
104.7 mins
BSTAR
0.000022276
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Other satellites on launch #238 in the year 2024 (2024-12-12 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.GJZ 01 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-09-16 11:14:05.552Z | 206.47° SW | 2025-09-16 11:18:05.552Z | 158.282° S | 43.198° | 2025-09-16 11:24:05.552Z | 43.493° NE |
| 8 mins | 2025-09-16 13:04:05.552Z | 280.152° WNW | 2025-09-16 13:08:05.552Z | 333.299° NNW | 24.891° | 2025-09-16 13:12:05.552Z | 18.439° NNE |
| 5 mins | 2025-09-16 16:48:05.552Z | 0.128° NNE | 2025-09-16 16:50:05.552Z | 21.248° NNE | 14.634° | 2025-09-16 16:53:05.552Z | 50.437° ENE |
| 10 mins | 2025-09-16 18:35:05.552Z | 335.211° NNW | 2025-09-16 18:40:05.552Z | 42.352° NE | 34.026° | 2025-09-16 18:45:05.552Z | 108.101° ESE |
| 10 mins | 2025-09-16 20:24:05.552Z | 301.91° NW | 2025-09-16 20:29:05.552Z | 228.376° WSW | 33.182° | 2025-09-16 20:34:05.552Z | 173.506° 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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