CZ-3B R/B, 62805
Orbit data source: Space-Track
CZ-3B R/B, 62805 is space debris in HEO originally from a launch on Thu, 23 Jan 2025 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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62805 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 | Unknown |
| Radar Cross Section | RCS unknown |
Expand to show TLE details & history
TLE from 1 day ago
0 CZ-3B R/B
1 62805U 25017B 25035.15265426 .00107769 68864-7 17119-2 0 9992
2 62805 28.4454 348.9603 7229121 186.3324 153.3145 2.39789477 271Epoch: 2025-02-04T03:39Z
Definitive object data (Epoch: 2025-02-04T03:39:49.328Z)
| Latitude | -0° |
| Longitude | 159.44213° |
| Altitude | 33,627.538 km |
| Speed | 1.739 km/s |
| True Right ascension | 23h 15m 50s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 28.43918° |
| Longitude | -115.82736° |
| Altitude | 6,714.698 km |
| Speed | 6.632 km/s |
| Apparent Right ascension | 03h 40m 32s |
| Apparent Declination | 15° 38' 15" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 06:54:14 |
| Azimuth | 254.239° W |
| Elevation | 41.537° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 34,251.907 km |
| Perigee altitude | 156.203 km |
| Semi-major axis | 23,582.192 km |
| Eccentricity | 0.7229121 |
| Inclination | 28.4454° |
| RAAN | 348.9603° |
| Arg. of periapsis | 186.3324° |
| True anomaly | 173.72406° |
| Mean anomaly | 153.3145° |
| Eccentric anomaly | 164.43131° |
| Mean motion | 0.59933 °/min |
| BSTAR | 0.0017119 |
| Orbital period | 600.67 mins |
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Other satellites on launch #17 in the year 2025 (2025-01-23 UTC)
| TJS-14, 62804 |
| CZ-3B R/B, 62805 |
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. |
|---|---|---|---|---|---|---|---|
| 21 mins | 2025-02-05 04:52:19.655Z | 254.142° W | 2025-02-05 05:04:19.655Z | 213.32° SW | 38.347° | 2025-02-05 05:13:19.655Z | 138.927° SSE |
| 496 mins | 2025-02-05 16:46:19.655Z | 144.348° SSE | 2025-02-06 00:15:19.655Z | 159.846° S | 42.326° | 2025-02-06 01:02:19.655Z | 92.676° ESE |
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