GJZ 02, 62291
Orbit data source: Space-Track
GJZ 02, 62291 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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62291 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 02
1 62291U 24238B 26036.31143309 .00000061 00000-0 18783-3 0 9997
2 62291 59.9179 289.8774 0008069 94.7658 265.4272 13.75180422 58148Epoch: 2026-02-05T07:28Z
TLE epoch observation values (Epoch: 2026-02-05T07:28:27.818Z)
Latitude
0.00001°
Longitude
42.29602°
Altitude
982.995 km
Speed
7.361 km/s
True Right ascension
19h 19m 30s
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
14:57:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
986.236 km
Perigee altitude
974.361 km
Semi-major axis
7,358.436 km
Eccentricity
0.00081
Inclination
59.9179°
RAAN
289.8774°
Arg. of periapsis
94.7658°
True anomaly
265.33504°
Mean anomaly
265.4272°
Eccentric anomaly
265.38112°
Mean motion
3.43847 °/min
Orbital period
104.7 mins
BSTAR
0.00018783
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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 02 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 | 2026-02-05 18:03:44.006Z | 181.06° SSW | 2026-02-05 18:08:44.006Z | 119.147° SE | 31.491° | 2026-02-05 18:13:44.006Z | 57.327° ENE |
| 10 mins | 2026-02-05 19:52:44.006Z | 251.527° W | 2026-02-05 19:56:44.006Z | 305.243° NW | 35.291° | 2026-02-05 20:02:44.006Z | 28.137° NE |
| 6 mins | 2026-02-05 21:44:44.006Z | 313.477° NW | 2026-02-05 21:47:44.006Z | 344.631° N | 15.281° | 2026-02-05 21:50:44.006Z | 14.007° NNE |
| 9 mins | 2026-02-06 01:25:44.006Z | 346.04° N | 2026-02-06 01:29:44.006Z | 34.652° NE | 24.147° | 2026-02-06 01:34:44.006Z | 88.251° E |
| 11 mins | 2026-02-06 03:13:44.006Z | 317.811° NNW | 2026-02-06 03:18:44.006Z | 245.682° WSW | 44.486° | 2026-02-06 03:24:44.006Z | 148.149° SSE |
| 4 mins | 2026-02-06 05:04:44.006Z | 266.185° W | 2026-02-06 05:06:44.006Z | 246.468° WSW | 12.771° | 2026-02-06 05:08:44.006Z | 227.389° WSW |
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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