GJZ 05, 62294
Orbit data source: Space-Track
GJZ 05, 62294 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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62294 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: 5 hours ago
TLE from 5 hours ago
0 GJZ 05
1 62294U 24238E 26036.31247551 .00000033 00000-0 15829-3 0 9991
2 62294 59.9132 310.1432 0009927 223.2590 136.7639 13.75185608 57773Epoch: 2026-02-05T07:29Z
TLE epoch observation values (Epoch: 2026-02-05T07:29:57.884Z)
Latitude
0°
Longitude
62.18551°
Altitude
987.824 km
Speed
7.356 km/s
True Right ascension
20h 40m 34s
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
14:58:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
987.586 km
Perigee altitude
972.976 km
Semi-major axis
7,358.418 km
Eccentricity
0.00099
Inclination
59.9132°
RAAN
310.1432°
Arg. of periapsis
223.259°
True anomaly
136.84175°
Mean anomaly
136.7639°
Eccentric anomaly
136.80283°
Mean motion
3.43848 °/min
Orbital period
104.7 mins
BSTAR
0.00015829
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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 05 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-02-05 19:49:50.903Z | 199.669° SSW | 2026-02-05 19:55:50.903Z | 119.002° SE | 40.364° | 2026-02-05 20:01:50.903Z | 46.668° ENE |
| 9 mins | 2026-02-05 21:40:50.903Z | 270.994° WNW | 2026-02-05 21:44:50.903Z | 326.832° NNW | 28.878° | 2026-02-05 21:49:50.903Z | 23.594° NE |
| 4 mins | 2026-02-05 23:33:50.903Z | 333.304° NNW | 2026-02-05 23:34:50.903Z | 343.262° N | 13.352° | 2026-02-05 23:37:50.903Z | 12.348° NNE |
| 5 mins | 2026-02-06 01:24:50.903Z | 355.879° N | 2026-02-06 01:26:50.903Z | 15.971° NNE | 13.76° | 2026-02-06 01:29:50.903Z | 44.443° NE |
| 10 mins | 2026-02-06 03:12:50.903Z | 340.856° N | 2026-02-06 03:16:50.903Z | 31.509° NE | 30.158° | 2026-02-06 03:22:50.903Z | 103.3° ESE |
| 11 mins | 2026-02-06 05:00:50.903Z | 309.226° NW | 2026-02-06 05:05:50.903Z | 242.137° WSW | 38.508° | 2026-02-06 05:11:50.903Z | 163.805° 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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