YAOGAN-31 C, 43277
Orbit data source: Space-Track
YAOGAN-31 C, 43277 is a payload satellite owned by PLA SSF (CN) in LEO that was launched on Tue, 10 Apr 2018 UTC via a CHANG ZHENG 4C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Payloads include a variety of satellites, spacecraft, and rockets 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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43277 intel report (Beta)
YAOGAN-31 C details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 4 hours ago |
| Origin | |
| Manufacturer | DFH |
| Mission | Operational Defense Sigint |
| Bus & Motor | Unknown |
| Mass | ~500 kg wet, ~500 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 1 m |
| Radar Cross Section | 0.446 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 4 hours ago
0 YAOGAN-31 C
1 43277U 18034C 24361.46330094 .00000068 00000-0 22872-3 0 9992
2 43277 63.3999 33.6788 0227455 5.5344 354.8117 13.45375508329896Epoch: 2024-12-26T11:07Z
Definitive object data (Epoch: 2024-12-26T11:07:09.201Z)
| Latitude | 0.00005° |
| Longitude | 131.44815° |
| Altitude | 921.95 km |
| Speed | 7.475 km/s |
| True Right ascension | 02h 14m 42s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 27.81027° |
| Longitude | -64.24871° |
| Altitude | 1,225.989 km |
| Speed | 7.179 km/s |
| Apparent Right ascension | 10h 26m 48s |
| Apparent Declination | -10° 15' 45" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 14:46:49 |
| Azimuth | 245.66° WSW |
| Elevation | 11.805° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,257.975 km |
| Perigee altitude | 918.326 km |
| Semi-major axis | 7,466.287 km |
| Eccentricity | 0.0227455 |
| Inclination | 63.3999° |
| RAAN | 33.6788° |
| Arg. of periapsis | 5.5344° |
| True anomaly | 354.56914° |
| Mean anomaly | 354.8117° |
| Eccentric anomaly | 354.69112° |
| Mean motion | 3.36423 °/min |
| BSTAR | 0.00022872 |
| Orbital period | 107.01 mins |
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Other satellites on launch #34 in the year 2018 (2018-04-10 UTC)
| YAOGAN-31 A, 43275 |
| YAOGAN-31 B, 43276 |
| YAOGAN-31 C, 43277 |
| CZ-4C R/B, 43278 |
| WEINA 1B, 43279 |
| CZ-4C DEB, 43280 |
| CZ-4C DEB, 43281 |
| CZ-4C DEB, 43338 |
| CZ-4C DEB, 44617 |
| CZ-4C DEB, 44618 |
| CZ-4C DEB, 45483 |
| CZ-4C DEB, 45484 |
YAOGAN-31 C Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2024-12-27 03:17:49.837Z | 167.99° S | 2024-12-27 03:21:49.837Z | 114.921° SE | 28.812° | 2024-12-27 03:26:49.837Z | 54.256° ENE |
| 10 mins | 2024-12-27 05:07:49.837Z | 247.383° WSW | 2024-12-27 05:11:49.837Z | 301.825° NW | 34.299° | 2024-12-27 05:17:49.837Z | 21.841° NNE |
| 9 mins | 2024-12-27 10:48:49.837Z | 357.003° N | 2024-12-27 10:52:49.837Z | 37.269° NE | 19.737° | 2024-12-27 10:57:49.837Z | 80.428° E |
| 13 mins | 2024-12-27 12:38:49.837Z | 330.965° NNW | 2024-12-27 12:43:49.837Z | 22.124° NNE | 43.702° | 2024-12-27 12:51:49.837Z | 140.458° SSE |
| 9 mins | 2024-12-27 14:30:49.837Z | 286.147° WNW | 2024-12-27 14:34:49.837Z | 245.337° WSW | 21.464° | 2024-12-27 14:39:49.837Z | 203.735° SW |
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