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: 10 hours ago
TLE from 10 hours ago
0 GJZ 04
1 62293U 24238D 26171.54745806 -.00000046 00000-0 76135-4 0 9994
2 62293 59.9137 260.8830 0014547 17.1412 343.0084 13.75200364 76378Epoch: 2026-06-20T13:08Z
TLE epoch observation values (Epoch: 2026-06-20T13:08:20.376Z)
Latitude
-0.00004°
Longitude
155.03757°
Altitude
972.208 km
Speed
7.371 km/s
True Right ascension
17h 23m 31s
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
10:18:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
990.932 km
Perigee altitude
969.524 km
Semi-major axis
7,358.365 km
Eccentricity
0.00145
Inclination
59.9137°
RAAN
260.883°
Arg. of periapsis
17.1412°
True anomaly
342.9596°
Mean anomaly
343.0084°
Eccentric anomaly
342.98401°
Mean motion
3.43852 °/min
Orbital period
104.7 mins
BSTAR
0.000076135
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-21 06:42:34.580Z | 160.178° S | 2026-06-21 06:46:34.580Z | 115.748° SE | 21.904° | 2026-06-21 06:50:34.580Z | 70.648° E |
| 11 mins | 2026-06-21 08:29:34.580Z | 231.949° WSW | 2026-06-21 08:34:34.580Z | 307.053° NW | 42.511° | 2026-06-21 08:40:34.580Z | 34.215° NE |
| 7 mins | 2026-06-21 10:21:34.580Z | 302.311° NW | 2026-06-21 10:24:34.580Z | 336.424° NNW | 18.667° | 2026-06-21 10:28:34.580Z | 17.222° NNE |
| 7 mins | 2026-06-21 14:03:34.580Z | 351.072° N | 2026-06-21 14:06:34.580Z | 24.311° NE | 19.388° | 2026-06-21 14:10:34.580Z | 67.664° E |
| 11 mins | 2026-06-21 15:51:34.580Z | 326.885° NNW | 2026-06-21 15:56:34.580Z | 57.572° ENE | 43.277° | 2026-06-21 16:02:34.580Z | 132.258° SE |
| 7 mins | 2026-06-21 17:41:34.580Z | 279.428° WNW | 2026-06-21 17:44:34.580Z | 243.74° WSW | 20.928° | 2026-06-21 17:48:34.580Z | 201.318° SSW |
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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