FLOCK 4BE 10, 60503
Orbit data source: Space-Track
FLOCK 4BE 10, 60503 is a payload satellite owned by Planet (US) in SSO that was launched on Fri, 16 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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60503 intel report (Beta)
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FLOCK 4BE 10 radio frequencies
FLOCK 4BE 10 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 21 hours ago |
| Origin | |
| Manufacturer | Planet |
| Mission | Operational spacecraft |
| 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 | Unknown |
| Radar Cross Section | Medium (>0.1 m² and <1 m²) |
Expand to show TLE details & history
TLE from 21 hours ago
0 FLOCK 4BE 10
1 60503U 24149AM 24355.69684704 .00013376 00000-0 58240-3 0 9999
2 60503 97.4314 69.5309 0004669 63.0775 297.0938 15.22335605 19122Epoch: 2024-12-20T16:43Z
Definitive object data (Epoch: 2024-12-20T16:43:27.584Z)
| Latitude | -0° |
| Longitude | 88.90732° |
| Altitude | 500.429 km |
| Speed | 7.615 km/s |
| True Right ascension | 04h 38m 07s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -27.4698° |
| Longitude | -94.07753° |
| Altitude | 511.812 km |
| Speed | 7.605 km/s |
| Apparent Right ascension | 19h 53m 40s |
| Apparent Declination | -57° 00' 39" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 13:10:29 |
| Azimuth | 137.216° SSE |
| Elevation | -38.055° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 498.971 km |
| Perigee altitude | 492.552 km |
| Semi-major axis | 6,873.899 km |
| Eccentricity | 0.0004669 |
| Inclination | 97.4314° |
| RAAN | 69.5309° |
| Arg. of periapsis | 63.0775° |
| True anomaly | 297.04616° |
| Mean anomaly | 297.0938° |
| Eccentric anomaly | 297.06998° |
| Mean motion | 3.80836 °/min |
| BSTAR | 0.0005824 |
| Orbital period | 94.53 mins |
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
FLOCK 4BE 10 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-21 18:32:25.188Z | 337.561° N | 2024-12-21 18:34:25.188Z | 277.073° WNW | 29.571° | 2024-12-21 18:37:25.188Z | 221.229° SW |
| 5 mins | 2024-12-22 05:09:25.188Z | 160.496° S | 2024-12-22 05:11:25.188Z | 11.012° NNE | 42.87° | 2024-12-22 05:14:25.188Z | 350.405° N |
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