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 26174.21680822 .00021672 00000-0 46620-3 0 9998
2 60563 97.3740 259.7517 0003637 250.5500 109.5356 15.44657586103356Epoch: 2026-06-23T05:12Z
TLE epoch observation values (Epoch: 2026-06-23T05:12:12.230Z)
Latitude
0.00002°
Longitude
-89.69081°
Altitude
436.338 km
Speed
7.65 km/s
True Right ascension
17h 19m 00s
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
20:00:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
431.792 km
Perigee altitude
426.84 km
Semi-major axis
6,807.453 km
Eccentricity
0.00036
Inclination
97.374°
RAAN
259.7517°
Arg. of periapsis
250.55°
True anomaly
109.57487°
Mean anomaly
109.5356°
Eccentric anomaly
109.55524°
Mean motion
3.86426 °/min
Orbital period
93.16 mins
BSTAR
0.0004662
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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 | 2026-06-24 19:05:38.201Z | 328.635° NNW | 2026-06-24 19:06:38.201Z | 295.405° NW | 28.402° | 2026-06-24 19:09:38.201Z | 222.636° SW |
| 5 mins | 2026-06-25 05:32:38.201Z | 144.722° SSE | 2026-06-25 05:34:38.201Z | 69.501° E | 38.269° | 2026-06-25 05:37:38.201Z | 358.67° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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