GUANGCHUAN 01, 62111
Orbit data source: Space-Track
GUANGCHUAN 01, 62111 is a payload satellite owned by Hongqing Keji (CN) in LEO that was launched on Wed, 27 Nov 2024 UTC via a ZHUQUE-2E 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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62111 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST?
Mission
Operational Commercial Communications
Bus & Motor
HQ, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.0 m
Radar Cross Section
4.560 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 GUANGCHUAN 01
1 62111U 24221A 26236.57499829 .00002024 00000-0 12294-3 0 9993
2 62111 49.9429 189.1021 0007011 219.3439 140.7003 15.15017710 96550Epoch: 2026-08-24T13:47Z
TLE epoch observation values (Epoch: 2026-08-24T13:47:59.852Z)
Latitude
-0.00001°
Longitude
9.24797°
Altitude
525.214 km
Speed
7.6 km/s
True Right ascension
12h 36m 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
14:55:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.541 km
Perigee altitude
516.866 km
Semi-major axis
6,899.84 km
Eccentricity
0.0007
Inclination
49.9429°
RAAN
189.1021°
Arg. of periapsis
219.3439°
True anomaly
140.75115°
Mean anomaly
140.7003°
Eccentric anomaly
140.72573°
Mean motion
3.78691 °/min
Orbital period
95.06 mins
BSTAR
0.00012294
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Other satellites on launch #221 in the year 2024 (2024-11-27 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.GUANGCHUAN 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-25 01:07:38.287Z | 272.517° WNW | 2026-08-25 01:10:38.287Z | 345.169° N | 31.457° | 2026-08-25 01:13:38.287Z | 42.299° NE |
| 4 mins | 2026-08-25 02:48:38.287Z | 322.149° NNW | 2026-08-25 02:50:38.287Z | 0.18° NNE | 18.345° | 2026-08-25 02:52:38.287Z | 35.052° NE |
| 5 mins | 2026-08-25 04:28:38.287Z | 334.081° NNW | 2026-08-25 04:30:38.287Z | 16.826° NNE | 23.018° | 2026-08-25 04:33:38.287Z | 70.605° E |
| 6 mins | 2026-08-25 06:07:38.287Z | 304.729° NW | 2026-08-25 06:10:38.287Z | 120.67° SE | 43.366° | 2026-08-25 06:13:38.287Z | 124.611° SE |
| 6 mins | 2026-08-25 23:13:38.287Z | 206.064° SW | 2026-08-25 23:15:38.287Z | 164.01° S | 34.927° | 2026-08-25 23:19:38.287Z | 66.981° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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