CZ-3A R/B, 43492
Orbit data source: Space-Track
CZ-3A R/B, 43492 is space debris originally from a launch on Tue, 05 Jun 2018 UTC launched from the Xichang Space Center, China (XSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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43492 intel report (Beta)
CZ-3A R/B details
| Identifier | |
| Orbit | Molniya |
| Last TLE update | 17 hours ago |
| Origin | |
| Manufacturer | CALT |
| Mission | Spacecraft |
| Bus & Motor | CZ-3A STAGE 3, Unknown motor |
| Mass | ~2,800 kg wet, ~2,800 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl + 1 Nozzle, 12.38 m |
| Radar Cross Section | 32.704 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 17 hours ago
0 CZ-3A R/B
1 43492U 18050B 24346.27345572 .00000754 00000-0 93087-3 0 9996
2 43492 24.4067 288.4200 7241748 241.2325 29.8161 2.28145613 53505Epoch: 2024-12-11T06:33Z
Definitive object data (Epoch: 2024-12-11T06:33:46.574Z)
| Latitude | 0.00007° |
| Longitude | 109.49537° |
| Altitude | 11,449.617 km |
| Speed | 5.326 km/s |
| True Right ascension | 19h 13m 38s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 23.80531° |
| Longitude | -174.57128° |
| Altitude | 31,902.711 km |
| Speed | 2.115 km/s |
| Apparent Right ascension | 00h 39m 40s |
| Apparent Declination | 19° 55' 57" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 21:43:36 |
| Azimuth | 104.777° ESE |
| Elevation | 47.499° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 35,654.02 km |
| Perigee altitude | 345.966 km |
| Semi-major axis | 24,378.13 km |
| Eccentricity | 0.7241748 |
| Inclination | 24.4067° |
| RAAN | 288.42° |
| Arg. of periapsis | 241.2325° |
| True anomaly | 119.03626° |
| Mean anomaly | 29.8161° |
| Eccentric anomaly | 68.39255° |
| Mean motion | 0.57022 °/min |
| BSTAR | 0.00093087 |
| Orbital period | 631.34 mins |
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Other satellites on launch #50 in the year 2018 (2018-06-05 UTC)
| FENGYUN 2H, 43491 |
| CZ-3A R/B, 43492 |
| FENGYUN 2H AKM, 43497 |
| FENGYUN 2H DEB, 43645 |
CZ-3A R/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. |
|---|---|---|---|---|---|---|---|
| 165 mins | 2024-12-11 23:19:26.724Z | 104.803° ESE | 2024-12-12 00:11:26.724Z | 106.617° ESE | 37.165° | 2024-12-12 02:04:26.724Z | 97.046° ESE |
| 109 mins | 2024-12-12 20:03:26.724Z | 75.08° E | 2024-12-12 21:06:26.724Z | 76.707° E | 12.243° | 2024-12-12 21:52:26.724Z | 76.677° E |
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