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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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4BE 19
1 60563U 24149CZ 26220.18086184 .00012379 00000-0 24976-3 0 9991
2 60563 97.3725 306.4662 0006163 108.6824 251.5095 15.46652198110452Epoch: 2026-08-08T04:20Z
TLE epoch observation values (Epoch: 2026-08-08T04:20:26.462Z)
Latitude
-0.00006°
Longitude
-75.33995°
Altitude
430.988 km
Speed
7.652 km/s
True Right ascension
20h 25m 51s
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
00:04:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
427.649 km
Perigee altitude
419.265 km
Semi-major axis
6,801.594 km
Eccentricity
0.00062
Inclination
97.3725°
RAAN
306.4662°
Arg. of periapsis
108.6824°
True anomaly
251.44254°
Mean anomaly
251.5095°
Eccentric anomaly
251.47602°
Mean motion
3.86925 °/min
Orbital period
93.04 mins
BSTAR
0.00024976
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-08 18:52:35.030Z | 1.442° NNE | 2026-08-08 18:54:35.030Z | 315.655° NNW | 39.873° | 2026-08-08 18:57:35.030Z | 204.994° SW |
| 4 mins | 2026-08-09 05:20:35.030Z | 112.001° ESE | 2026-08-09 05:21:35.030Z | 83.526° E | 24.584° | 2026-08-09 05:24:35.030Z | 12.851° NNE |
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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