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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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 01
1 62290U 24238A 26036.31260473 -.00000032 00000-0 90175-4 0 9993
2 62290 59.9153 325.8248 0025170 134.8561 225.4497 13.75195251 57462Epoch: 2026-02-05T07:30Z
TLE epoch observation values (Epoch: 2026-02-05T07:30:09.048Z)
Latitude
-0.00004°
Longitude
77.82044°
Altitude
995.482 km
Speed
7.348 km/s
True Right ascension
21h 43m 17s
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
998.767 km
Perigee altitude
961.725 km
Semi-major axis
7,358.383 km
Eccentricity
0.00252
Inclination
59.9153°
RAAN
325.8248°
Arg. of periapsis
134.8561°
True anomaly
225.24461°
Mean anomaly
225.4497°
Eccentric anomaly
225.34711°
Mean motion
3.4385 °/min
Orbital period
104.7 mins
BSTAR
0.000090175
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-05 19:49:51.426Z | 157.911° S | 2026-02-05 19:53:51.426Z | 118.101° SE | 19.346° | 2026-02-05 19:57:51.426Z | 74.565° E |
| 11 mins | 2026-02-05 21:36:51.426Z | 226.159° WSW | 2026-02-05 21:41:51.426Z | 286.879° WNW | 43.854° | 2026-02-05 21:47:51.426Z | 35.859° NE |
| 7 mins | 2026-02-05 23:28:51.426Z | 298.7° NW | 2026-02-05 23:31:51.426Z | 334.046° NNW | 19.984° | 2026-02-05 23:35:51.426Z | 16.38° NNE |
| 7 mins | 2026-02-06 03:10:51.426Z | 350.181° N | 2026-02-06 03:13:51.426Z | 22.404° NNE | 17.808° | 2026-02-06 03:17:51.426Z | 64.506° ENE |
| 11 mins | 2026-02-06 04:58:51.426Z | 328.997° NNW | 2026-02-06 05:03:51.426Z | 47.551° ENE | 41.447° | 2026-02-06 05:09:51.426Z | 127.25° SE |
| 8 mins | 2026-02-06 06:48:51.426Z | 283.347° WNW | 2026-02-06 06:51:51.426Z | 245.543° WSW | 23.3° | 2026-02-06 06:56:51.426Z | 191.732° 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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