FLOCK 4V 13, 46297 (Decayed)
Orbit data source: Space-Track
FLOCK 4V 13, 46297 was a payload satellite owned by Planet (US) in LEO that was launched on Thu, 03 Sep 2020 UTC via a VEGA launch vehicle from the French Guiana (FRGUI). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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46297 intel report (Beta)
FLOCK 4V 13 details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 1 month ago |
| Origin | |
| Manufacturer | Planet |
| Mission | Decayed Commercial Imaging |
| Bus & Motor | CUBESAT 3U, Unknown motor |
| Mass | 5.7 kg wet, 5.7 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 0.3 m |
| Radar Cross Section | 0.108 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 1 month ago
0 FLOCK 4V 13
1 46297U 20061AB 24329.45292653 .17114732 24962-5 53868-3 0 9990
2 46297 97.2954 47.8657 0013161 277.7576 82.2231 16.43721337234842Epoch: 2024-11-24T10:52Z
Definitive object data (Epoch: 2024-11-24T10:52:12.852Z)
| Latitude | -0.00003° |
| Longitude | -179.07924° |
| Altitude | 158.028 km |
| Speed | 7.812 km/s |
| True Right ascension | 03h 11m 27s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
| Apogee altitude | 161.315 km |
| Perigee altitude | 144.125 km |
| Semi-major axis | 6,530.857 km |
| Eccentricity | 0.0013161 |
| Inclination | 97.2954° |
| RAAN | 47.8657° |
| Arg. of periapsis | 277.7576° |
| True anomaly | 82.37256° |
| Mean anomaly | 82.2231° |
| Eccentric anomaly | 82.29783° |
| Mean motion | 4.11233 °/min |
| BSTAR | 0.00053868 |
| Orbital period | 87.54 mins |
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Other satellites on launch #61 in the year 2020 (2020-09-03 UTC)
FLOCK 4V 13 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. |
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