CZ-2C R/B, 62078
Orbit data source: Space-Track
CZ-2C R/B, 62078 is space debris in SSO originally from a launch on Sun, 24 Nov 2024 UTC via a CHANG ZHENG 2C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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62078 intel report (Beta)
CZ-2C R/B details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 8 hours ago |
| Origin | |
| Manufacturer | CALT |
| Mission | Spacecraft |
| Bus & Motor | CZ-2 STAGE 2, Unknown motor |
| Mass | ~3,800 kg wet, ~3,800 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| 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 8 hours ago
0 CZ-2C R/B
1 62078U 24218A 24361.07624793 .00011248 00000-0 58050-3 0 9991
2 62078 97.5503 5.5121 0055549 84.5739 276.1826 15.15129452 4711Epoch: 2024-12-26T01:49Z
Definitive object data (Epoch: 2024-12-26T01:49:47.821Z)
| Latitude | -0.00006° |
| Longitude | -116.99798° |
| Altitude | 519.748 km |
| Speed | 7.606 km/s |
| True Right ascension | 00h 22m 02s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 77.08329° |
| Longitude | 98.43092° |
| Altitude | 497.005 km |
| Speed | 7.643 km/s |
| Apparent Right ascension | 20h 19m 49s |
| Apparent Declination | 28° 27' 15" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 09:32:46 |
| Azimuth | 16.976° NNE |
| Elevation | -19.557° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 555.869 km |
| Perigee altitude | 479.259 km |
| Semi-major axis | 6,895.701 km |
| Eccentricity | 0.0055549 |
| Inclination | 97.5503° |
| RAAN | 5.5121° |
| Arg. of periapsis | 84.5739° |
| True anomaly | 275.5493° |
| Mean anomaly | 276.1826° |
| Eccentric anomaly | 275.86599° |
| Mean motion | 3.79032 °/min |
| BSTAR | 0.0005805 |
| Orbital period | 94.98 mins |
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Other satellites on launch #218 in the year 2024 (2024-11-24 UTC)
| CZ-2C R/B, 62078 |
| SUPERVIEW NEO-2 03, 62079 |
| SUPERVIEW NEO-2 04, 62080 |
CZ-2C 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2024-12-26 13:28:37.550Z | 9.25° NNE | 2024-12-26 13:31:37.550Z | 344.578° N | 42.776° | 2024-12-26 13:35:37.550Z | 197.18° SSW |
| 4 mins | 2024-12-27 00:10:37.550Z | 123.833° SE | 2024-12-27 00:11:37.550Z | 94.463° ESE | 31.591° | 2024-12-27 00:14:37.550Z | 8.966° NNE |
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