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: 8 hours ago
TLE from 8 hours ago
0 GJZ 04
1 62293U 24238D 25291.30874590 -.00000054 00000-0 68101-4 0 9996
2 62293 59.9129 283.1408 0019700 135.4093 224.8503 13.75157408 42648Epoch: 2025-10-18T07:24Z
TLE epoch observation values (Epoch: 2025-10-18T07:24:35.645Z)
Latitude
-0.00009°
Longitude
144.95061°
Altitude
992.891 km
Speed
7.351 km/s
True Right ascension
18h 52m 33s
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
09:58:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
994.878 km
Perigee altitude
965.885 km
Semi-major axis
7,358.518 km
Eccentricity
0.00197
Inclination
59.9129°
RAAN
283.1408°
Arg. of periapsis
135.4093°
True anomaly
224.69137°
Mean anomaly
224.8503°
Eccentric anomaly
224.77081°
Mean motion
3.43841 °/min
Orbital period
104.7 mins
BSTAR
0.000068101
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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 | 2025-10-19 00:58:19.350Z | 191.477° SSW | 2025-10-19 01:04:19.350Z | 114.087° SE | 35.959° | 2025-10-19 01:09:19.350Z | 52.614° ENE |
| 10 mins | 2025-10-19 02:48:19.350Z | 259.259° W | 2025-10-19 02:52:19.350Z | 311.066° NW | 31.974° | 2025-10-19 02:58:19.350Z | 26.688° NE |
| 5 mins | 2025-10-19 04:41:19.350Z | 325.395° NNW | 2025-10-19 04:43:19.350Z | 345.984° N | 14.125° | 2025-10-19 04:46:19.350Z | 14.856° NNE |
| 9 mins | 2025-10-19 08:21:19.350Z | 345.292° N | 2025-10-19 08:25:19.350Z | 37.464° NE | 26.779° | 2025-10-19 08:30:19.350Z | 94.158° ESE |
| 11 mins | 2025-10-19 10:09:19.350Z | 313.086° NW | 2025-10-19 10:14:19.350Z | 228.868° WSW | 42.214° | 2025-10-19 10:20:19.350Z | 155.428° 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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