FLOCK 4BE 24, 60505
Orbit data source: Space-Track
FLOCK 4BE 24, 60505 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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60505 intel report (Beta)
FLOCK 4BE 24 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 19 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 19 hours ago
0 FLOCK 4BE 24
1 60505U 24149AP 24355.79360510 .00014254 00000-0 60807-3 0 9996
2 60505 97.4252 69.5888 0006484 64.7213 295.4694 15.23006632 19148Epoch: 2024-12-20T19:02Z
Definitive object data (Epoch: 2024-12-20T19:02:47.48Z)
| Latitude | -0.00013° |
| Longitude | 54.03697° |
| Altitude | 497.957 km |
| Speed | 7.617 km/s |
| True Right ascension | 04h 38m 21s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 41.97105° |
| Longitude | 48.12935° |
| Altitude | 498.718 km |
| Speed | 7.622 km/s |
| Apparent Right ascension | 02h 45m 08s |
| Apparent Declination | 3° 08' 17" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 13:11:15 |
| Azimuth | 327.729° NNW |
| Elevation | -41.864° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 498.196 km |
| Perigee altitude | 489.285 km |
| Semi-major axis | 6,871.877 km |
| Eccentricity | 0.0006484 |
| Inclination | 97.4252° |
| RAAN | 69.5888° |
| Arg. of periapsis | 64.7213° |
| True anomaly | 295.4023° |
| Mean anomaly | 295.4694° |
| Eccentric anomaly | 295.43585° |
| Mean motion | 3.81004 °/min |
| BSTAR | 0.00060807 |
| Orbital period | 94.49 mins |
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
FLOCK 4BE 24 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2024-12-21 17:41:11.060Z | 27.229° NE | 2024-12-21 17:44:11.060Z | 100.855° ESE | 35.825° | 2024-12-21 17:47:11.060Z | 171.668° S |
| 4 mins | 2024-12-22 05:53:11.060Z | 231.711° WSW | 2024-12-22 05:54:11.060Z | 257.088° W | 23.08° | 2024-12-22 05:57:11.060Z | 318.896° NNW |
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