FLOCK 4BE 12, 60560
Orbit data source: Space-Track
FLOCK 4BE 12, 60560 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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60560 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Non-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: 13 hours ago
TLE from 13 hours ago
0 FLOCK 4BE 12
1 60560U 24149CW 26133.19118984 .00089532 00000-0 94489-3 0 9997
2 60560 97.3657 219.1577 0002458 158.7446 201.3916 15.63931975 97098Epoch: 2026-05-13T04:35Z
TLE epoch observation values (Epoch: 2026-05-13T04:35:18.802Z)
Latitude
0.00005°
Longitude
-80.62541°
Altitude
381.009 km
Speed
7.68 km/s
True Right ascension
14h 36m 37s
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
01:52:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
374.877 km
Perigee altitude
371.558 km
Semi-major axis
6,751.355 km
Eccentricity
0.00025
Inclination
97.3657°
RAAN
219.1577°
Arg. of periapsis
158.7446°
True anomaly
201.38133°
Mean anomaly
201.3916°
Eccentric anomaly
201.38646°
Mean motion
3.91252 °/min
Orbital period
92.01 mins
BSTAR
0.00094489
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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 12 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 | 2026-05-13 18:57:26.579Z | 353.375° N | 2026-05-13 19:00:26.579Z | 261.465° W | 29.087° | 2026-05-13 19:02:26.579Z | 218.749° SW |
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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