FLOCK 4BE 19, 60563
Orbit data source: Space-Track
FLOCK 4BE 19, 60563 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). Payload-class satellites include a variety of spacecraft 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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60563 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Operational 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
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.072 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4BE 19
1 60563U 24149CZ 25310.20786180 .00024275 00000-0 72639-3 0 9993
2 60563 97.3961 28.7899 0004879 28.3296 331.8212 15.34530007 68112Epoch: 2025-11-06T04:59Z
TLE epoch observation values (Epoch: 2025-11-06T04:59:19.259Z)
Latitude
0.00003°
Longitude
-91.70983°
Altitude
462.485 km
Speed
7.637 km/s
True Right ascension
01h 55m 09s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
09:55:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.599 km
Perigee altitude
455.927 km
Semi-major axis
6,837.4 km
Eccentricity
0.00049
Inclination
97.3961°
RAAN
28.7899°
Arg. of periapsis
28.3296°
True anomaly
331.79478°
Mean anomaly
331.8212°
Eccentric anomaly
331.80799°
Mean motion
3.8389 °/min
Orbital period
93.78 mins
BSTAR
0.00072639
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.FLOCK 4BE 19 Visibility forecast
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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 | 2025-11-06 18:03:49.381Z | 19.545° NNE | 2025-11-06 18:06:49.381Z | 81.449° E | 41.022° | 2025-11-06 18:09:49.381Z | 180.554° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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