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: 6 hours ago
TLE from 6 hours ago
0 GJZ 01
1 62290U 24238A 25346.20147240 .00000062 00000-0 18808-3 0 9994
2 62290 59.9117 132.6316 0028291 103.6280 256.7881 13.75181595 49888Epoch: 2025-12-12T04:50Z
TLE epoch observation values (Epoch: 2025-12-12T04:50:07.215Z)
Latitude
-0.00002°
Longitude
-21.04497°
Altitude
987.326 km
Speed
7.356 km/s
True Right ascension
08h 50m 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
09:00:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,001.113 km
Perigee altitude
959.478 km
Semi-major axis
7,358.432 km
Eccentricity
0.00283
Inclination
59.9117°
RAAN
132.6316°
Arg. of periapsis
103.628°
True anomaly
256.47275°
Mean anomaly
256.7881°
Eccentric anomaly
256.6304°
Mean motion
3.43847 °/min
Orbital period
104.7 mins
BSTAR
0.00018808
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-12-12 11:56:45.926Z | 208.347° SW | 2025-12-12 12:02:45.926Z | 89.458° E | 43.18° | 2025-12-12 12:07:45.926Z | 43.439° NE |
| 8 mins | 2025-12-12 13:47:45.926Z | 279.731° WNW | 2025-12-12 13:51:45.926Z | 332.055° NNW | 24.922° | 2025-12-12 13:55:45.926Z | 17.846° NNE |
| 5 mins | 2025-12-12 17:31:45.926Z | 359.425° N | 2025-12-12 17:33:45.926Z | 20.553° NNE | 14.544° | 2025-12-12 17:36:45.926Z | 50.043° ENE |
| 9 mins | 2025-12-12 19:19:45.926Z | 340.37° N | 2025-12-12 19:23:45.926Z | 41.195° NE | 33.987° | 2025-12-12 19:28:45.926Z | 108.209° ESE |
| 10 mins | 2025-12-12 21:07:45.926Z | 301.983° NW | 2025-12-12 21:12:45.926Z | 229.121° WSW | 32.839° | 2025-12-12 21:17:45.926Z | 173.768° 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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