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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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: 4 hours ago
TLE from 4 hours ago
0 GJZ 01
1 62290U 24238A 26311.28023001 -.00000029 00000-0 93688-4 0 9997
2 62290 59.9129 213.5236 0022396 23.1687 337.0326 13.75241179 95285Epoch: 2026-11-07T06:43Z
TLE epoch observation values (Epoch: 2026-11-07T06:43:31.872Z)
Latitude
0.00001°
Longitude
66.15305°
Altitude
967.13 km
Speed
7.376 km/s
True Right ascension
14h 14m 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
07:12:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
996.562 km
Perigee altitude
963.603 km
Semi-major axis
7,358.22 km
Eccentricity
0.00224
Inclination
59.9129°
RAAN
213.5236°
Arg. of periapsis
23.1687°
True anomaly
336.9322°
Mean anomaly
337.0326°
Eccentric anomaly
336.98243°
Mean motion
3.43862 °/min
Orbital period
104.69 mins
BSTAR
0.000093688
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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 | 2026-11-07 19:02:58.893Z | 190.156° SSW | 2026-11-07 19:08:58.893Z | 113.145° SE | 44.444° | 2026-11-07 19:13:58.893Z | 53.027° ENE |
| 10 mins | 2026-11-07 20:52:58.893Z | 258.466° W | 2026-11-07 20:56:58.893Z | 312.288° NW | 39.587° | 2026-11-07 21:02:58.893Z | 27.223° NE |
| 5 mins | 2026-11-07 22:45:58.893Z | 326.052° NNW | 2026-11-07 22:47:58.893Z | 346.837° N | 14.759° | 2026-11-07 22:50:58.893Z | 15.433° NNE |
| 9 mins | 2026-11-08 02:25:58.893Z | 346.368° N | 2026-11-08 02:29:58.893Z | 38.168° NE | 29.833° | 2026-11-08 02:34:58.893Z | 93.107° ESE |
| 11 mins | 2026-11-08 04:13:58.893Z | 314.076° NW | 2026-11-08 04:18:58.893Z | 226.53° WSW | 68.45° | 2026-11-08 04:24:58.893Z | 153.892° SSE |
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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