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: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4BE 19
1 60563U 24149CZ 26296.03548348 .00030816 00000-0 52532-3 0 9998
2 60563 97.3679 23.8630 0004709 179.0782 181.0480 15.51301869122195Epoch: 2026-10-23T00:51Z
TLE epoch observation values (Epoch: 2026-10-23T00:51:05.772Z)
Latitude
-0°
Longitude
-20.37286°
Altitude
419.256 km
Speed
7.658 km/s
True Right ascension
01h 35m 27s
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
06:42:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
413.043 km
Perigee altitude
406.65 km
Semi-major axis
6,787.984 km
Eccentricity
0.00047
Inclination
97.3679°
RAAN
23.863°
Arg. of periapsis
179.0782°
True anomaly
181.04701°
Mean anomaly
181.048°
Eccentric anomaly
181.04751°
Mean motion
3.8809 °/min
Orbital period
92.76 mins
BSTAR
0.00052532
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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 | 2026-10-23 18:26:48.442Z | 36.49° NE | 2026-10-23 18:28:48.442Z | 85.165° E | 33.122° | 2026-10-23 18:31:48.442Z | 164.056° S |
| 5 mins | 2026-10-24 06:23:48.442Z | 194.283° SSW | 2026-10-24 06:25:48.442Z | 246.707° WSW | 40.255° | 2026-10-24 06:28:48.442Z | 331.546° NNW |
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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