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: 13 hours ago
TLE from 13 hours ago
0 GJZ 04
1 62293U 24238D 25340.89511747 -.00000101 00000-0 19015-4 0 9990
2 62293 59.9114 133.0621 0015417 163.3649 196.7868 13.75167295 49463Epoch: 2025-12-06T21:28Z
TLE epoch observation values (Epoch: 2025-12-06T21:28:58.149Z)
Latitude
0.00002°
Longitude
94.90353°
Altitude
993.427 km
Speed
7.35 km/s
True Right ascension
08h 52m 14s
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
08:39:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
991.691 km
Perigee altitude
969.002 km
Semi-major axis
7,358.483 km
Eccentricity
0.00154
Inclination
59.9114°
RAAN
133.0621°
Arg. of periapsis
163.3649°
True anomaly
196.73587°
Mean anomaly
196.7868°
Eccentric anomaly
196.76133°
Mean motion
3.43843 °/min
Orbital period
104.7 mins
BSTAR
0.000019015
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-12-07 11:33:40.056Z | 181.98° SSW | 2025-12-07 11:38:40.056Z | 120.351° SE | 32.102° | 2025-12-07 11:43:40.056Z | 57.241° ENE |
| 10 mins | 2025-12-07 13:22:40.056Z | 251.966° W | 2025-12-07 13:27:40.056Z | 329.925° NNW | 35.011° | 2025-12-07 13:32:40.056Z | 27.608° NE |
| 6 mins | 2025-12-07 15:14:40.056Z | 312.963° NW | 2025-12-07 15:17:40.056Z | 343.732° N | 15.289° | 2025-12-07 15:20:40.056Z | 13.28° NNE |
| 9 mins | 2025-12-07 18:55:40.056Z | 345.159° N | 2025-12-07 18:59:40.056Z | 33.311° NE | 24.403° | 2025-12-07 19:04:40.056Z | 88.272° E |
| 11 mins | 2025-12-07 20:43:40.056Z | 317.413° NNW | 2025-12-07 20:48:40.056Z | 253.091° W | 44.265° | 2025-12-07 20:54:40.056Z | 149.015° 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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