GJZ 01, 62290
Orbit data source: Space-Track
GJZ 01, 62290 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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62290 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 01
1 62290U 24238A 26126.24869612 -.00000034 00000-0 87864-4 0 9998
2 62290 59.9145 53.6002 0016357 199.1605 160.8789 13.75214955 69830Epoch: 2026-05-06T05:58Z
TLE epoch observation values (Epoch: 2026-05-06T05:58:07.344Z)
Latitude
-0.00008°
Longitude
99.95765°
Altitude
993.769 km
Speed
7.35 km/s
True Right ascension
03h 34m 24s
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
19:36:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
992.212 km
Perigee altitude
968.14 km
Semi-major axis
7,358.313 km
Eccentricity
0.00164
Inclination
59.9145°
RAAN
53.6002°
Arg. of periapsis
199.1605°
True anomaly
160.94018°
Mean anomaly
160.8789°
Eccentric anomaly
160.90955°
Mean motion
3.43855 °/min
Orbital period
104.7 mins
BSTAR
0.000087864
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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 01 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 20:02:22.618Z | 170.047° S | 2026-05-06 20:07:22.618Z | 115.055° SE | 25.148° | 2026-05-06 20:12:22.618Z | 61.716° ENE |
| 11 mins | 2026-05-06 21:50:22.618Z | 237.384° WSW | 2026-05-06 21:55:22.618Z | 309.495° NW | 40.682° | 2026-05-06 22:01:22.618Z | 32.4° NE |
| 7 mins | 2026-05-06 23:42:22.618Z | 303.918° NW | 2026-05-06 23:45:22.618Z | 336.192° NNW | 17.766° | 2026-05-06 23:49:22.618Z | 16.557° NNE |
| 8 mins | 2026-05-07 03:24:22.618Z | 349.978° N | 2026-05-07 03:27:22.618Z | 23.66° NE | 20.669° | 2026-05-07 03:32:22.618Z | 77.103° E |
| 11 mins | 2026-05-07 05:12:22.618Z | 324.069° NNW | 2026-05-07 05:17:22.618Z | 62.649° ENE | 44.484° | 2026-05-07 05:23:22.618Z | 137.164° SSE |
| 6 mins | 2026-05-07 07:02:22.618Z | 277.31° WNW | 2026-05-07 07:05:22.618Z | 243.957° WSW | 18.008° | 2026-05-07 07:08:22.618Z | 212.187° SW |
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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