FLOCK 4BE 2, 60511
Orbit data source: Space-Track
FLOCK 4BE 2, 60511 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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60511 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: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4BE 2
1 60511U 24149AV 26316.20269035 .00506836 00000-0 17511-2 0 9993
2 60511 97.3687 50.2718 0003118 300.4341 59.6623 15.88319583125646Epoch: 2026-11-12T04:51Z
TLE epoch observation values (Epoch: 2026-11-12T04:51:52.446Z)
Latitude
0.00002°
Longitude
-74.03629°
Altitude
309.125 km
Speed
7.723 km/s
True Right ascension
03h 21m 05s
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
12:43:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
305.951 km
Perigee altitude
301.784 km
Semi-major axis
6,682.005 km
Eccentricity
0.00031
Inclination
97.3687°
RAAN
50.2718°
Arg. of periapsis
300.4341°
True anomaly
59.69314°
Mean anomaly
59.6623°
Eccentric anomaly
59.67772°
Mean motion
3.97359 °/min
Orbital period
90.6 mins
BSTAR
0.0017511
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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 2 Visibility
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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. |
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| FLOCK 4BE 2 is likely not visible in the next few days. |
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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