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: 12 hours ago
TLE from 12 hours ago
0 GUANGCHUAN 01
1 62111U 24221A 26072.15782015 .00005930 00000-0 32269-3 0 9990
2 62111 49.9440 269.4339 0007203 269.6018 90.4108 15.15691552 71632Epoch: 2026-03-13T03:47Z
TLE epoch observation values (Epoch: 2026-03-13T03:47:15.660Z)
Latitude
-0.00001°
Longitude
41.82126°
Altitude
519.465 km
Speed
7.605 km/s
True Right ascension
17h 57m 44s
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
20:17:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
524.627 km
Perigee altitude
514.69 km
Semi-major axis
6,897.795 km
Eccentricity
0.00072
Inclination
49.944°
RAAN
269.4339°
Arg. of periapsis
269.6018°
True anomaly
90.49334°
Mean anomaly
90.4108°
Eccentric anomaly
90.45207°
Mean motion
3.78859 °/min
Orbital period
95.02 mins
BSTAR
0.00032269
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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 | 2026-03-13 16:39:43.513Z | 250.06° W | 2026-03-13 16:42:43.513Z | 334.68° NNW | 41.659° | 2026-03-13 16:45:43.513Z | 48.529° ENE |
| 4 mins | 2026-03-13 18:20:43.513Z | 313.683° NW | 2026-03-13 18:22:43.513Z | 355.502° N | 20.448° | 2026-03-13 18:24:43.513Z | 31.759° NE |
| 4 mins | 2026-03-13 20:00:43.513Z | 332.991° NNW | 2026-03-13 20:02:43.513Z | 11.845° NNE | 19.415° | 2026-03-13 20:04:43.513Z | 48.582° ENE |
| 6 mins | 2026-03-13 21:39:43.513Z | 317.497° NNW | 2026-03-13 21:42:43.513Z | 44.932° NE | 36.989° | 2026-03-13 21:45:43.513Z | 102.599° ESE |
| 5 mins | 2026-03-13 23:19:43.513Z | 264.436° W | 2026-03-13 23:21:43.513Z | 216.899° SW | 24.273° | 2026-03-13 23:24:43.513Z | 166.868° S |
| 4 mins | 2026-03-14 14:46:43.513Z | 164.457° S | 2026-03-14 14:47:43.513Z | 142.878° SSE | 21.63° | 2026-03-14 14:50:43.513Z | 85.453° E |
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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