YAOGAN-31 B, 43276
Orbit data source: Space-Track
YAOGAN-31 B, 43276 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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43276 intel report (Beta)
YAOGAN-31 B 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 B
1 43276U 18034B 24361.46345199 .00000070 00000-0 23163-3 0 9990
2 43276 63.3990 34.3725 0227352 5.7475 354.6079 13.45375262329878Epoch: 2024-12-26T11:07Z
Definitive object data (Epoch: 2024-12-26T11:07:22.251Z)
| Latitude | -0.00006° |
| Longitude | 132.08728° |
| Altitude | 922.085 km |
| Speed | 7.474 km/s |
| True Right ascension | 02h 17m 29s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 62.32789° |
| Longitude | -156.52083° |
| Altitude | 1,053.922 km |
| Speed | 7.353 km/s |
| Apparent Right ascension | 04h 17m 53s |
| Apparent Declination | 19° 44' 25" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 14:26:48 |
| Azimuth | 331.067° NNW |
| Elevation | -24.962° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,257.899 km |
| Perigee altitude | 918.404 km |
| Semi-major axis | 7,466.288 km |
| Eccentricity | 0.0227352 |
| Inclination | 63.399° |
| RAAN | 34.3725° |
| Arg. of periapsis | 5.7475° |
| True anomaly | 354.35596° |
| Mean anomaly | 354.6079° |
| Eccentric anomaly | 354.48266° |
| Mean motion | 3.36423 °/min |
| BSTAR | 0.00023163 |
| 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 B 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-26 15:20:51.425Z | 278.425° WNW | 2024-12-26 15:23:51.425Z | 254.303° W | 12.577° | 2024-12-26 15:25:51.425Z | 238.226° WSW |
| 8 mins | 2024-12-27 03:18:51.425Z | 159.593° S | 2024-12-27 03:21:51.425Z | 116.962° SE | 27.795° | 2024-12-27 03:26:51.425Z | 55.658° ENE |
| 10 mins | 2024-12-27 05:07:51.425Z | 245.273° WSW | 2024-12-27 05:12:51.425Z | 325.196° NNW | 34.954° | 2024-12-27 05:17:51.425Z | 21.967° NNE |
| 9 mins | 2024-12-27 10:48:51.425Z | 356.434° N | 2024-12-27 10:52:51.425Z | 36.092° NE | 19.288° | 2024-12-27 10:57:51.425Z | 79.134° E |
| 13 mins | 2024-12-27 12:38:51.425Z | 331.577° NNW | 2024-12-27 12:44:51.425Z | 81.24° E | 43.424° | 2024-12-27 12:51:51.425Z | 139.009° SSE |
| 9 mins | 2024-12-27 14:30:51.425Z | 287.611° WNW | 2024-12-27 14:34:51.425Z | 246.343° WSW | 22.285° | 2024-12-27 14:39:51.425Z | 203.282° SW |
Authenticating...
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