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 26125.87657189 .00004164 00000-0 24002-3 0 9995
2 62111 49.9452 8.0914 0007305 128.2477 231.9132 15.14367540 79771Epoch: 2026-05-05T21:02Z
TLE epoch observation values (Epoch: 2026-05-05T21:02:15.811Z)
Latitude
0°
Longitude
-171.2196°
Altitude
526.557 km
Speed
7.599 km/s
True Right ascension
00h 32m 21s
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
14:29:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.719 km
Perigee altitude
518.635 km
Semi-major axis
6,901.814 km
Eccentricity
0.00073
Inclination
49.9452°
RAAN
8.0914°
Arg. of periapsis
128.2477°
True anomaly
231.84735°
Mean anomaly
231.9132°
Eccentric anomaly
231.88027°
Mean motion
3.78528 °/min
Orbital period
95.11 mins
BSTAR
0.00024002
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-06 17:47:00.923Z | 169.242° S | 2026-05-06 17:49:00.923Z | 135.913° SSE | 16.847° | 2026-05-06 17:51:00.923Z | 100.069° ESE |
| 6 mins | 2026-05-06 19:26:00.923Z | 247.795° W | 2026-05-06 19:28:00.923Z | 315.522° NNW | 43.479° | 2026-05-06 19:32:00.923Z | 52.782° ENE |
| 5 mins | 2026-05-06 21:06:00.923Z | 308.458° NW | 2026-05-06 21:08:00.923Z | 350.269° N | 21.268° | 2026-05-06 21:11:00.923Z | 40.289° NE |
| 4 mins | 2026-05-06 22:47:00.923Z | 344.671° N | 2026-05-06 22:48:00.923Z | 5.098° NNE | 18.775° | 2026-05-06 22:51:00.923Z | 55.42° ENE |
| 5 mins | 2026-05-07 00:26:00.923Z | 325.645° NNW | 2026-05-07 00:28:00.923Z | 23.244° NE | 35.029° | 2026-05-07 00:31:00.923Z | 96.001° ESE |
| 5 mins | 2026-05-07 02:05:00.923Z | 274.813° WNW | 2026-05-07 02:07:00.923Z | 230.892° WSW | 27.139° | 2026-05-07 02:10:00.923Z | 166.45° S |
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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