GJZ 04, 62293
Orbit data source: Space-Track
GJZ 04, 62293 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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62293 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: 5 hours ago
TLE from 5 hours ago
0 GJZ 04
1 62293U 24238D 26036.31443306 .00000039 00000-0 16434-3 0 9995
2 62293 59.9150 310.1967 0008510 217.0785 142.9636 13.75181094 57770Epoch: 2026-02-05T07:32Z
TLE epoch observation values (Epoch: 2026-02-05T07:32:47.016Z)
Latitude
0.00001°
Longitude
61.53237°
Altitude
987.515 km
Speed
7.356 km/s
True Right ascension
20h 40m 47s
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
14:57:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
986.559 km
Perigee altitude
974.035 km
Semi-major axis
7,358.434 km
Eccentricity
0.00085
Inclination
59.915°
RAAN
310.1967°
Arg. of periapsis
217.0785°
True anomaly
143.02229°
Mean anomaly
142.9636°
Eccentric anomaly
142.99295°
Mean motion
3.43847 °/min
Orbital period
104.7 mins
BSTAR
0.00016434
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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 04 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 | 2026-02-05 19:52:43.636Z | 201.253° SSW | 2026-02-05 19:58:43.636Z | 120.033° SE | 41.086° | 2026-02-05 20:04:43.636Z | 46.052° ENE |
| 9 mins | 2026-02-05 21:43:43.636Z | 271.841° WNW | 2026-02-05 21:47:43.636Z | 326.098° NNW | 28.258° | 2026-02-05 21:52:43.636Z | 23.071° NE |
| 4 mins | 2026-02-05 23:36:43.636Z | 333.066° NNW | 2026-02-05 23:37:43.636Z | 342.928° N | 13.132° | 2026-02-05 23:40:43.636Z | 12.021° NNE |
| 5 mins | 2026-02-06 01:27:43.636Z | 355.501° N | 2026-02-06 01:29:43.636Z | 15.631° NNE | 13.936° | 2026-02-06 01:32:43.636Z | 44.472° NE |
| 10 mins | 2026-02-06 03:15:43.636Z | 340.161° N | 2026-02-06 03:19:43.636Z | 30.676° NE | 30.743° | 2026-02-06 03:25:43.636Z | 104.332° ESE |
| 10 mins | 2026-02-06 05:04:43.636Z | 304.33° NW | 2026-02-06 05:08:43.636Z | 242.668° WSW | 37.66° | 2026-02-06 05:14:43.636Z | 165.341° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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