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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4BE 2
1 60511U 24149AV 26035.19950578 .00025680 00000-0 64390-3 0 9999
2 60511 97.3907 120.0046 0003811 54.6342 305.5260 15.40017840 81954Epoch: 2026-02-04T04:47Z
TLE epoch observation values (Epoch: 2026-02-04T04:47:17.299Z)
Latitude
0.00001°
Longitude
-86.18699°
Altitude
447.664 km
Speed
7.644 km/s
True Right ascension
08h 00m 01s
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
12:25:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
445.595 km
Perigee altitude
440.396 km
Semi-major axis
6,821.132 km
Eccentricity
0.00038
Inclination
97.3907°
RAAN
120.0046°
Arg. of periapsis
54.6342°
True anomaly
305.49045°
Mean anomaly
305.526°
Eccentric anomaly
305.50823°
Mean motion
3.85264 °/min
Orbital period
93.44 mins
BSTAR
0.0006439
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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 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 | 2026-02-04 17:50:27.029Z | 48.848° ENE | 2026-02-04 17:52:27.029Z | 99.8° ESE | 23.922° | 2026-02-04 17:54:27.029Z | 147.433° SSE |
| 5 mins | 2026-02-05 05:52:27.029Z | 190.066° SSW | 2026-02-05 05:54:27.029Z | 249.266° W | 37.075° | 2026-02-05 05:57:27.029Z | 335.114° 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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