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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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: 6 hours ago
TLE from 6 hours ago
0 GJZ 04
1 62293U 24238D 26126.25187539 .00000002 00000-0 12592-3 0 9992
2 62293 59.9153 37.9803 0010456 342.3457 17.7186 13.75193394 70147Epoch: 2026-05-06T06:02Z
TLE epoch observation values (Epoch: 2026-05-06T06:02:42.033Z)
Latitude
-0.00003°
Longitude
83.1901°
Altitude
975.141 km
Speed
7.368 km/s
True Right ascension
02h 31m 55s
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
19:36:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
987.947 km
Perigee altitude
972.559 km
Semi-major axis
7,358.39 km
Eccentricity
0.00105
Inclination
59.9153°
RAAN
37.9803°
Arg. of periapsis
342.3457°
True anomaly
17.75511°
Mean anomaly
17.7186°
Eccentric anomaly
17.73685°
Mean motion
3.4385 °/min
Orbital period
104.7 mins
BSTAR
0.00012592
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-06 18:23:23.986Z | 137.541° SSE | 2026-05-06 18:26:23.986Z | 108.921° ESE | 13.139° | 2026-05-06 18:28:23.986Z | 89.457° E |
| 10 mins | 2026-05-06 20:09:23.986Z | 211.635° SW | 2026-05-06 20:13:23.986Z | 177.724° S | 44.104° | 2026-05-06 20:19:23.986Z | 41.501° NE |
| 8 mins | 2026-05-06 21:59:23.986Z | 282.325° WNW | 2026-05-06 22:03:23.986Z | 332.187° NNW | 23.883° | 2026-05-06 22:07:23.986Z | 17.103° NNE |
| 5 mins | 2026-05-07 01:43:23.986Z | 358.838° N | 2026-05-07 01:45:23.986Z | 20.057° NNE | 15.667° | 2026-05-07 01:48:23.986Z | 50.401° ENE |
| 11 mins | 2026-05-07 03:30:23.986Z | 333.31° NNW | 2026-05-07 03:35:23.986Z | 38.89° NE | 36.084° | 2026-05-07 03:41:23.986Z | 115.137° SE |
| 10 mins | 2026-05-07 05:19:23.986Z | 300.071° NW | 2026-05-07 05:24:23.986Z | 232.53° WSW | 30.946° | 2026-05-07 05:29:23.986Z | 177.902° 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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