CZ-3B R/B, 61504
Orbit data source: Space-Track
CZ-3B R/B, 61504 is space debris in HEO originally from a launch on Thu, 10 Oct 2024 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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61504 intel report (Beta)
CZ-3B R/B details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 3 weeks 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 3 weeks ago
0 CZ-3B R/B
1 61504U 24181B 24334.66049471 .01267368 10382-5 21845-2 0 9999
2 61504 28.3128 203.3678 7007776 212.8130 72.1581 2.70806288 1154Epoch: 2024-11-29T15:51Z
Definitive object data (Epoch: 2024-11-29T15:51:06.742Z)
| Latitude | 0° |
| Longitude | -103.39156° |
| Altitude | 20,541.666 km |
| Speed | 3.359 km/s |
| True Right ascension | 13h 33m 38s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -2.73657° |
| Longitude | -120.13273° |
| Altitude | 10,789.652 km |
| Speed | 5.029 km/s |
| Apparent Right ascension | 11h 22m 25s |
| Apparent Declination | -17° 45' 38" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 16:24:53 |
| Azimuth | 247.307° WSW |
| Elevation | -0.819° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 30,606.184 km |
| Perigee altitude | 128.615 km |
| Semi-major axis | 21,745.537 km |
| Eccentricity | 0.7007776 |
| Inclination | 28.3128° |
| RAAN | 203.3678° |
| Arg. of periapsis | 212.813° |
| True anomaly | 147.21334° |
| Mean anomaly | 72.1581° |
| Eccentric anomaly | 109.90983° |
| Mean motion | 0.67684 °/min |
| BSTAR | 0.0021845 |
| Orbital period | 531.88 mins |
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Other satellites on launch #181 in the year 2024 (2024-10-10 UTC)
| HG-03, 61503 |
| CZ-3B R/B, 61504 |
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. |
|---|---|---|---|---|---|---|---|
| 350 mins | 2024-12-21 17:40:16.630Z | 247.195° WSW | 2024-12-21 23:10:16.630Z | 224.424° SW | 38.094° | 2024-12-21 23:30:16.630Z | 152.462° SSE |
| 130 mins | 2024-12-22 15:12:16.630Z | 222.213° SW | 2024-12-22 17:22:16.630Z | 221.944° SW | 39.645° | 2024-12-22 17:22:16.630Z | 221.944° SW |
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