CZ-7A R/B, 60607
Orbit data source: Space-Track
CZ-7A R/B, 60607 is space debris in HEO originally from a launch on Thu, 22 Aug 2024 UTC launched from the Wenchang Satellite Launch Center (WSC). 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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60607 intel report (Beta)
CZ-7A R/B details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 4 months 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 4 months ago
0 CZ-7A R/B
1 60607U 24151B 24261.03072416 .01161033 20484-5 27794-2 0 9999
2 60607 14.6562 169.5289 6954656 190.0106 140.9887 2.77671165 530Epoch: 2024-09-17T00:44Z
Definitive object data (Epoch: 2024-09-17T00:44:14.567Z)
| Latitude | 0.00022° |
| Longitude | 162.05089° |
| Altitude | 28,678.843 km |
| Speed | 2.025 km/s |
| True Right ascension | 11h 18m 15s |
| True Declination | 0° 00' 01" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -0.27849° |
| Longitude | -118.79033° |
| Altitude | 4,141.342 km |
| Speed | 5.786 km/s |
| Apparent Right ascension | 17h 46m 49s |
| Apparent Declination | -16° 46' 36" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 08:32:58 |
| Azimuth | 69.411° E |
| Elevation | -47.298° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 29,882.813 km |
| Perigee altitude | 134.945 km |
| Semi-major axis | 21,387.016 km |
| Eccentricity | 0.6954656 |
| Inclination | 14.6562° |
| RAAN | 169.5289° |
| Arg. of periapsis | 190.0106° |
| True anomaly | 170.02557° |
| Mean anomaly | 140.9887° |
| Eccentric anomaly | 156.73057° |
| Mean motion | 0.69393 °/min |
| BSTAR | 0.0027794 |
| Orbital period | 518.78 mins |
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Other satellites on launch #151 in the year 2024 (2024-08-22 UTC)
| CHINASAT 4A, 60606 |
| CZ-7A R/B, 60607 |
CZ-7A 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. |
|---|---|---|---|---|---|---|---|
| 131 mins | 2025-01-15 09:31:21.421Z | 224.812° SW | 2025-01-15 10:11:21.421Z | 166.996° S | 33.234° | 2025-01-15 11:42:21.421Z | 122.961° SE |
| 102 mins | 2025-01-15 14:50:21.421Z | 253.022° W | 2025-01-15 15:50:21.421Z | 225.825° WSW | 19.8° | 2025-01-15 16:32:21.421Z | 190.32° SSW |
| 59 mins | 2025-01-16 06:54:21.421Z | 168.45° S | 2025-01-16 07:10:21.421Z | 135.031° SSE | 18.897° | 2025-01-16 07:53:21.421Z | 107.36° ESE |
Authenticating...
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