CZ-3B R/B, 42663
Orbit data source: Space-Track
CZ-3B R/B, 42663 is space debris in HEO originally from a launch on Wed, 12 Apr 2017 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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42663 intel report (Beta)
CZ-3B R/B details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 1 day 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 1 day ago
0 CZ-3B R/B
1 42663U 17018B 24339.38136709 .00012298 00000-0 15707-2 0 9990
2 42663 20.6768 359.8671 6951464 330.9890 3.8430 2.72272443 62669Epoch: 2024-12-04T09:09Z
Definitive object data (Epoch: 2024-12-04T09:09:10.116Z)
| Latitude | 0.00008° |
| Longitude | 148.89132° |
| Altitude | 606.351 km |
| Speed | 9.784 km/s |
| True Right ascension | 23h 59m 26s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 1.78172° |
| Longitude | -36.31143° |
| Altitude | 24,664.947 km |
| Speed | 2.698 km/s |
| Apparent Right ascension | 12h 14m 04s |
| Apparent Declination | -5° 59' 46" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 07:04:54 |
| Azimuth | 102.806° ESE |
| Elevation | 5.785° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 30,352.578 km |
| Perigee altitude | 227.482 km |
| Semi-major axis | 21,668.167 km |
| Eccentricity | 0.6951464 |
| Inclination | 20.6768° |
| RAAN | 359.8671° |
| Arg. of periapsis | 330.989° |
| True anomaly | 28.70676° |
| Mean anomaly | 3.843° |
| Eccentric anomaly | 12.38656° |
| Mean motion | 0.68047 °/min |
| BSTAR | 0.0015707 |
| Orbital period | 529.04 mins |
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Other satellites on launch #18 in the year 2017 (2017-04-12 UTC)
| CHINASAT 16, 42662 |
| CZ-3B R/B, 42663 |
CZ-3B 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. |
|---|---|---|---|---|---|---|---|
| 326 mins | 2024-12-05 12:19:44.224Z | 270.726° WNW | 2024-12-05 13:47:44.224Z | 254.512° W | 27.97° | 2024-12-05 17:45:44.224Z | 254.355° W |
| 223 mins | 2024-12-06 05:23:44.224Z | 207.725° SW | 2024-12-06 05:38:44.224Z | 144.569° SSE | 35.475° | 2024-12-06 09:06:44.224Z | 116.64° SE |
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