FLOCK 4BE 30, 60499
Orbit data source: Space-Track
FLOCK 4BE 30, 60499 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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60499 intel report (Beta)
FLOCK 4BE 30 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 20 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 20 hours ago
0 FLOCK 4BE 30
1 60499U 24149AH 24355.75423306 .00014681 00000-0 63252-3 0 9998
2 60499 97.4324 69.6172 0004743 55.7038 304.4647 15.22671448 18519Epoch: 2024-12-20T18:06Z
Definitive object data (Epoch: 2024-12-20T18:06:05.736Z)
| Latitude | -0.00001° |
| Longitude | 68.27809° |
| Altitude | 499.035 km |
| Speed | 7.616 km/s |
| True Right ascension | 04h 38m 28s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 21.31414° |
| Longitude | -108.01187° |
| Altitude | 501.373 km |
| Speed | 7.615 km/s |
| Apparent Right ascension | 19h 59m 05s |
| Apparent Declination | -14° 52' 13" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:45:16 |
| Azimuth | 90.032° ESE |
| Elevation | -23.537° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 498.01 km |
| Perigee altitude | 491.49 km |
| Semi-major axis | 6,872.887 km |
| Eccentricity | 0.0004743 |
| Inclination | 97.4324° |
| RAAN | 69.6172° |
| Arg. of periapsis | 55.7038° |
| True anomaly | 304.41987° |
| Mean anomaly | 304.4647° |
| Eccentric anomaly | 304.44229° |
| Mean motion | 3.80921 °/min |
| BSTAR | 0.00063252 |
| Orbital period | 94.51 mins |
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
FLOCK 4BE 30 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 18:19:16.108Z | 357.777° N | 2024-12-21 18:22:16.108Z | 267.554° W | 37.387° | 2024-12-21 18:25:16.108Z | 210.049° SW |
| 5 mins | 2024-12-22 04:56:16.108Z | 146.894° SSE | 2024-12-22 04:58:16.108Z | 103.887° ESE | 37.23° | 2024-12-22 05:01:16.108Z | 2.154° NNE |
Authenticating...
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