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: 10 hours ago
TLE from 10 hours ago
0 GJZ 04
1 62293U 24238D 25258.59023520 -.00000057 00000-0 64330-4 0 9992
2 62293 59.9154 22.1640 0022243 117.5559 242.7712 13.75149498 38140Epoch: 2025-09-15T14:09Z
TLE epoch observation values (Epoch: 2025-09-15T14:09:56.321Z)
Latitude
-0°
Longitude
174.88662°
Altitude
990.145 km
Speed
7.354 km/s
True Right ascension
01h 28m 39s
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
16:48:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
996.777 km
Perigee altitude
964.042 km
Semi-major axis
7,358.546 km
Eccentricity
0.00222
Inclination
59.9154°
RAAN
22.164°
Arg. of periapsis
117.5559°
True anomaly
242.54485°
Mean anomaly
242.7712°
Eccentric anomaly
242.65799°
Mean motion
3.43839 °/min
Orbital period
104.7 mins
BSTAR
0.00006433
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-09-16 09:28:15.484Z | 182.504° SSW | 2025-09-16 09:33:15.484Z | 128.255° SE | 30.877° | 2025-09-16 09:39:15.484Z | 55.133° ENE |
| 10 mins | 2025-09-16 11:17:15.484Z | 248.806° W | 2025-09-16 11:22:15.484Z | 320.393° NNW | 35.837° | 2025-09-16 11:27:15.484Z | 26.599° NE |
| 5 mins | 2025-09-16 13:10:15.484Z | 318.664° NNW | 2025-09-16 13:12:15.484Z | 339.865° N | 15.341° | 2025-09-16 13:15:15.484Z | 10.451° NNE |
| 8 mins | 2025-09-16 16:51:15.484Z | 351.075° N | 2025-09-16 16:54:15.484Z | 28.456° NE | 23.682° | 2025-09-16 16:59:15.484Z | 85.488° E |
| 10 mins | 2025-09-16 18:39:15.484Z | 317.689° NNW | 2025-09-16 18:43:15.484Z | 285.588° WNW | 43.952° | 2025-09-16 18:49:15.484Z | 147.733° 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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