CZ-3B R/B, 62486
Orbit data source: Space-Track
CZ-3B R/B, 62486 is space debris in HEO originally from a launch on Mon, 06 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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62486 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 | Large (>1 m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 CZ-3B R/B
1 62486U 25002B 25034.78996571 .00041406 98827-6 76024-3 0 9998
2 62486 28.5690 33.8249 7350818 195.9190 114.1308 2.24149856 631Epoch: 2025-02-03T18:57Z
Definitive object data (Epoch: 2025-02-03T18:57:33.037Z)
| Latitude | -0.00016° |
| Longitude | -24.77545° |
| Altitude | 32,299.425 km |
| Speed | 2.109 km/s |
| True Right ascension | 02h 15m 16s |
| True Declination | 0° 00' 01" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 11.61166° |
| Longitude | -3.13795° |
| Altitude | 35,220.742 km |
| Speed | 1.731 km/s |
| Apparent Right ascension | 03h 15m 25s |
| Apparent Declination | 6° 16' 37" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 08:06:50 |
| Azimuth | 263.741° W |
| Elevation | 17.152° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 36,420.445 km |
| Perigee altitude | 156.496 km |
| Semi-major axis | 24,666.608 km |
| Eccentricity | 0.7350818 |
| Inclination | 28.569° |
| RAAN | 33.8249° |
| Arg. of periapsis | 195.919° |
| True anomaly | 164.14382° |
| Mean anomaly | 114.1308° |
| Eccentric anomaly | 140.76816° |
| Mean motion | 0.56025 °/min |
| BSTAR | 0.00076024 |
| Orbital period | 642.57 mins |
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Other satellites on launch #2 in the year 2025 (2025-01-06 UTC)
| SJ-25, 62485 |
| CZ-3B R/B, 62486 |
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. |
|---|---|---|---|---|---|---|---|
| 247 mins | 2025-02-05 06:04:44.015Z | 263.725° W | 2025-02-05 10:04:44.015Z | 237.212° WSW | 25.914° | 2025-02-05 10:11:44.015Z | 187.061° SSW |
| 487 mins | 2025-02-05 21:57:44.015Z | 186.897° SSW | 2025-02-06 02:16:44.015Z | 211.83° SW | 36.651° | 2025-02-06 06:04:44.015Z | 254.38° W |
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