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: 17 hours ago
TLE from 17 hours ago
0 GJZ 01
1 62290U 24238A 25301.63223961 .00000028 00000-0 15249-3 0 9995
2 62290 59.9130 267.5289 0028160 78.7080 281.7090 13.75168021 43754Epoch: 2025-10-28T15:10Z
TLE epoch observation values (Epoch: 2025-10-28T15:10:25.502Z)
Latitude
-0.00001°
Longitude
2.70569°
Altitude
978.411 km
Speed
7.365 km/s
True Right ascension
17h 50m 06s
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
03:16:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,001.065 km
Perigee altitude
959.622 km
Semi-major axis
7,358.481 km
Eccentricity
0.00282
Inclination
59.913°
RAAN
267.5289°
Arg. of periapsis
78.708°
True anomaly
281.3928°
Mean anomaly
281.709°
Eccentric anomaly
281.55092°
Mean motion
3.43844 °/min
Orbital period
104.7 mins
BSTAR
0.00015249
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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 | 2025-10-29 09:12:02.749Z | 303.758° NW | 2025-10-29 09:18:02.749Z | 232.914° WSW | 29.148° | 2025-10-29 09:23:02.749Z | 179.922° S |
| 9 mins | 2025-10-29 22:43:02.749Z | 166.341° S | 2025-10-29 22:47:02.749Z | 112.07° ESE | 27.177° | 2025-10-29 22:52:02.749Z | 58.638° ENE |
| 11 mins | 2025-10-30 00:30:02.749Z | 242.346° WSW | 2025-10-30 00:35:02.749Z | 316.429° NNW | 38.54° | 2025-10-30 00:41:02.749Z | 31.575° NE |
| 6 mins | 2025-10-30 02:22:02.749Z | 306.809° NW | 2025-10-30 02:25:02.749Z | 338.558° N | 16.304° | 2025-10-30 02:28:02.749Z | 9.953° NNE |
| 8 mins | 2025-10-30 06:04:02.749Z | 351.507° N | 2025-10-30 06:07:02.749Z | 27.287° NE | 21.728° | 2025-10-30 06:12:02.749Z | 81.361° E |
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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