CZ-3A R/B, 43492
Orbit data source: Space-Track
CZ-3A R/B, 43492 is space debris in HEO 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 | HEO |
| Last TLE update | 2 days 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 2 days ago
0 CZ-3A R/B
1 43492U 18050B 24359.85364674 .00000671 00000-0 89374-3 0 9990
2 43492 24.3821 283.3433 7239573 249.9060 23.9892 2.28164336 53811Epoch: 2024-12-24T20:29Z
Definitive object data (Epoch: 2024-12-24T20:29:15.078Z)
| Latitude | 0.00039° |
| Longitude | -117.78254° |
| Altitude | 9,114.258 km |
| Speed | 5.925 km/s |
| True Right ascension | 18h 53m 32s |
| True Declination | 0° 00' 01" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 24.35824° |
| Longitude | -32.43483° |
| Altitude | 32,007.977 km |
| Speed | 2.101 km/s |
| Apparent Right ascension | 00h 15m 30s |
| Apparent Declination | 16° 51' 44" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 09:46:43 |
| Azimuth | 320.889° NNW |
| Elevation | -23.488° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 35,646.417 km |
| Perigee altitude | 350.899 km |
| Semi-major axis | 24,376.795 km |
| Eccentricity | 0.7239573 |
| Inclination | 24.3821° |
| RAAN | 283.3433° |
| Arg. of periapsis | 249.906° |
| True anomaly | 110.39958° |
| Mean anomaly | 23.9892° |
| Eccentric anomaly | 59.86139° |
| Mean motion | 0.57027 °/min |
| BSTAR | 0.00089374 |
| Orbital period | 631.28 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. |
|---|---|---|---|---|---|---|---|
| 324 mins | 2024-12-26 17:54:32.270Z | 77.937° E | 2024-12-26 21:39:32.270Z | 87.376° E | 24.718° | 2024-12-26 23:18:32.270Z | 86.846° E |
| 227 mins | 2024-12-27 01:59:32.270Z | 266.297° W | 2024-12-27 03:20:32.270Z | 272.582° WNW | 16.529° | 2024-12-27 05:46:32.270Z | 284.946° WNW |
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