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: 14 hours ago
TLE from 14 hours ago
0 GJZ 01
1 62290U 24238A 25260.33445712 -.00000083 00000-0 37920-4 0 9999
2 62290 59.9149 32.5212 0026797 56.1079 304.2473 13.75157884 38072Epoch: 2025-09-17T08:01Z
TLE epoch observation values (Epoch: 2025-09-17T08:01:37.095Z)
Latitude
0.00005°
Longitude
-84.39523°
Altitude
971.534 km
Speed
7.372 km/s
True Right ascension
02h 10m 05s
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
15:04:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,000.098 km
Perigee altitude
960.661 km
Semi-major axis
7,358.517 km
Eccentricity
0.00268
Inclination
59.9149°
RAAN
32.5212°
Arg. of periapsis
56.1079°
True anomaly
303.99299°
Mean anomaly
304.2473°
Eccentric anomaly
304.12019°
Mean motion
3.43841 °/min
Orbital period
104.7 mins
BSTAR
0.00003792
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-09-18 10:18:39.153Z | 196.269° SSW | 2025-09-18 10:24:39.153Z | 124.284° SE | 38.069° | 2025-09-18 10:30:39.153Z | 48.649° ENE |
| 9 mins | 2025-09-18 12:09:39.153Z | 266.885° W | 2025-09-18 12:13:39.153Z | 325.221° NNW | 30.138° | 2025-09-18 12:18:39.153Z | 24.23° NE |
| 4 mins | 2025-09-18 14:02:39.153Z | 332.391° NNW | 2025-09-18 14:03:39.153Z | 342.62° N | 13.4° | 2025-09-18 14:06:39.153Z | 12.111° NNE |
| 4 mins | 2025-09-18 15:53:39.153Z | 355.767° N | 2025-09-18 15:55:39.153Z | 15.778° NNE | 12.946° | 2025-09-18 15:57:39.153Z | 35.188° NE |
| 9 mins | 2025-09-18 17:41:39.153Z | 341.993° N | 2025-09-18 17:45:39.153Z | 31.934° NE | 28.33° | 2025-09-18 17:50:39.153Z | 95.073° ESE |
| 11 mins | 2025-09-18 19:29:39.153Z | 311.555° NW | 2025-09-18 19:34:39.153Z | 243.535° WSW | 40.537° | 2025-09-18 19:40:39.153Z | 159.827° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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