BEIDOU 3M16, 43648
Orbit data source: Space-Track
BEIDOU 3M16, 43648 is a payload satellite owned by CNSA (CN) in MEO that was launched on Mon, 15 Oct 2018 UTC via a CHANG ZHENG 3B/YZ-1 launch vehicle from the Xichang Space Center, China (XSC). 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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43648 intel report (Beta)
BEIDOU 3M16 details
| Identifier | |
| Orbit | MEO |
| Last TLE update | 21 hours ago |
| Origin | |
| Manufacturer | SECM |
| Mission | Operational Defense Navigation |
| Bus & Motor | BD-3M/SAR, Unknown motor |
| Mass | 1,014 kg wet, ~850 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 10 m |
| Radar Cross Section | 8.984 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 21 hours ago
0 BEIDOU 3M16
1 43648U 18078B 24336.42679671 -.00000062 00000-0 00000-0 0 9998
2 43648 54.5819 319.6367 0003632 4.0268 355.9736 1.86232212 41693Epoch: 2024-12-01T10:14Z
Definitive object data (Epoch: 2024-12-01T10:14:35.235Z)
| Latitude | -0.00002° |
| Longitude | 95.20952° |
| Altitude | 21,518.11 km |
| Speed | 3.781 km/s |
| True Right ascension | 21h 18m 29s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -44.04171° |
| Longitude | -41.42622° |
| Altitude | 21,549.201 km |
| Speed | 3.778 km/s |
| Apparent Right ascension | 13h 03m 19s |
| Apparent Declination | -47° 22' 20" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 05:26:06 |
| Azimuth | 121.986° SE |
| Elevation | -43.307° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 21,538.089 km |
| Perigee altitude | 21,517.818 km |
| Semi-major axis | 27,906.091 km |
| Eccentricity | 0.0003632 |
| Inclination | 54.5819° |
| RAAN | 319.6367° |
| Arg. of periapsis | 4.0268° |
| True anomaly | 355.97068° |
| Mean anomaly | 355.9736° |
| Eccentric anomaly | 355.97214° |
| Mean motion | 0.46558 °/min |
| BSTAR | Unknown |
| Orbital period | 773.23 mins |
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Other satellites on launch #78 in the year 2018 (2018-10-15 UTC)
| BEIDOU 3M15, 43647 |
| BEIDOU 3M16, 43648 |
| CZ-3B R/B, 43649 |
| YZ-1 R/B, 43650 |
BEIDOU 3M16 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. |
|---|---|---|---|---|---|---|---|
| 441 mins | 2024-12-02 23:51:59.861Z | 203.42° SW | 2024-12-03 03:03:59.861Z | 314.118° NW | 44.536° | 2024-12-03 07:12:59.861Z | 106.711° ESE |
Authenticating...
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