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: 1 day ago
TLE from 1 day ago
0 FLOCK 4BE 19
1 60563U 24149CZ 26259.04464738 .00043289 00000-0 80911-3 0 9998
2 60563 97.3697 346.0518 0003702 325.5656 34.5355 15.48615368116464Epoch: 2026-09-16T01:04Z
TLE epoch observation values (Epoch: 2026-09-16T01:04:17.533Z)
Latitude
0.00004°
Longitude
-25.02315°
Altitude
421.832 km
Speed
7.659 km/s
True Right ascension
23h 04m 12s
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
05:13:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
420.218 km
Perigee altitude
415.186 km
Semi-major axis
6,795.839 km
Eccentricity
0.00037
Inclination
97.3697°
RAAN
346.0518°
Arg. of periapsis
325.5656°
True anomaly
34.55956°
Mean anomaly
34.5355°
Eccentric anomaly
34.54753°
Mean motion
3.87417 °/min
Orbital period
92.92 mins
BSTAR
0.00080911
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-17 17:58:00.284Z | 56.709° ENE | 2026-09-17 18:00:00.284Z | 97.703° ESE | 16.548° | 2026-09-17 18:02:00.284Z | 136.248° SSE |
| 5 mins | 2026-09-18 05:56:00.284Z | 164.067° S | 2026-09-18 05:58:00.284Z | 115.542° SE | 81.64° | 2026-09-18 06:01:00.284Z | 349.822° N |
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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