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 26252.20995011 .00002362 00000-0 14348-3 0 9992
2 62111 49.9429 112.9752 0007083 278.8400 81.1748 15.14309687 98925Epoch: 2026-09-09T05:02Z
TLE epoch observation values (Epoch: 2026-09-09T05:02:19.689Z)
Latitude
-0.00004°
Longitude
49.12784°
Altitude
522.874 km
Speed
7.604 km/s
True Right ascension
07h 31m 54s
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
07:05:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.742 km
Perigee altitude
518.964 km
Semi-major axis
6,901.99 km
Eccentricity
0.00071
Inclination
49.9429°
RAAN
112.9752°
Arg. of periapsis
278.84°
True anomaly
81.25502°
Mean anomaly
81.1748°
Eccentric anomaly
81.21491°
Mean motion
3.78514 °/min
Orbital period
95.11 mins
BSTAR
0.00014348
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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 | 2026-09-09 17:54:26.297Z | 229.227° WSW | 2026-09-09 17:57:26.297Z | 91.38° ESE | 74.076° | 2026-09-09 18:00:26.297Z | 58.138° ENE |
| 5 mins | 2026-09-09 19:34:26.297Z | 293.963° NW | 2026-09-09 19:36:26.297Z | 333.328° NNW | 26.674° | 2026-09-09 19:39:26.297Z | 34.447° NE |
| 4 mins | 2026-09-09 21:15:26.297Z | 333.243° NNW | 2026-09-09 21:17:26.297Z | 11.695° NNE | 19.039° | 2026-09-09 21:19:26.297Z | 44.447° NE |
| 6 mins | 2026-09-09 22:54:26.297Z | 323.728° NNW | 2026-09-09 22:57:26.297Z | 33.643° NE | 34.081° | 2026-09-09 23:00:26.297Z | 87.345° E |
| 5 mins | 2026-09-10 00:34:26.297Z | 283.21° WNW | 2026-09-10 00:36:26.297Z | 223.618° SW | 48.293° | 2026-09-10 00:39:26.297Z | 150.1° SSE |
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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