GJZ 03, 62292
Orbit data source: Space-Track
GJZ 03, 62292 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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62292 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 03
1 62292U 24238C 26126.24778353 .00000007 00000-0 13083-3 0 9991
2 62292 59.9152 37.9567 0014537 325.9142 34.0931 13.75200936 70123Epoch: 2026-05-06T05:56Z
TLE epoch observation values (Epoch: 2026-05-06T05:56:48.496Z)
Latitude
-0.00005°
Longitude
84.6436°
Altitude
973.588 km
Speed
7.37 km/s
True Right ascension
02h 31m 49s
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
19:35:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
990.923 km
Perigee altitude
969.529 km
Semi-major axis
7,358.363 km
Eccentricity
0.00145
Inclination
59.9152°
RAAN
37.9567°
Arg. of periapsis
325.9142°
True anomaly
34.18662°
Mean anomaly
34.0931°
Eccentric anomaly
34.13984°
Mean motion
3.43852 °/min
Orbital period
104.7 mins
BSTAR
0.00013083
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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 03 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 | 2026-05-06 20:03:22.758Z | 207.178° SW | 2026-05-06 20:07:22.758Z | 156.35° SSE | 43.571° | 2026-05-06 20:13:22.758Z | 43.109° NE |
| 8 mins | 2026-05-06 21:53:22.758Z | 281.096° WNW | 2026-05-06 21:57:22.758Z | 333.839° NNW | 24.998° | 2026-05-06 22:01:22.758Z | 18.385° NNE |
| 4 mins | 2026-05-06 23:46:22.758Z | 338.257° N | 2026-05-06 23:47:22.758Z | 347.969° N | 12.49° | 2026-05-06 23:50:22.758Z | 16.236° NNE |
| 5 mins | 2026-05-07 01:37:22.758Z | 359.889° N | 2026-05-07 01:39:22.758Z | 20.919° NNE | 15.142° | 2026-05-07 01:42:22.758Z | 50.223° ENE |
| 11 mins | 2026-05-07 03:24:22.758Z | 334.827° NNW | 2026-05-07 03:29:22.758Z | 40.982° NE | 34.601° | 2026-05-07 03:35:22.758Z | 112.508° SE |
| 10 mins | 2026-05-07 05:13:22.758Z | 301.706° NW | 2026-05-07 05:18:22.758Z | 230.215° WSW | 32.995° | 2026-05-07 05:23:22.758Z | 174.553° 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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