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: 15 hours ago
TLE from 15 hours ago
0 FLOCK 4BE 2
1 60511U 24149AV 25289.19694362 .00019785 00000-0 59961-3 0 9992
2 60511 97.4042 8.2921 0004506 90.9435 269.2324 15.34170532 64906Epoch: 2025-10-16T04:43Z
TLE epoch observation values (Epoch: 2025-10-16T04:43:35.928Z)
Latitude
-0.00005°
Longitude
-87.56772°
Altitude
466.538 km
Speed
7.633 km/s
True Right ascension
00h 33m 10s
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
14:41:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.414 km
Perigee altitude
457.251 km
Semi-major axis
6,838.469 km
Eccentricity
0.00045
Inclination
97.4042°
RAAN
8.2921°
Arg. of periapsis
90.9435°
True anomaly
269.18077°
Mean anomaly
269.2324°
Eccentric anomaly
269.20658°
Mean motion
3.838 °/min
Orbital period
93.8 mins
BSTAR
0.00059961
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-17 05:54:39.628Z | 206.824° SW | 2025-10-17 05:56:39.628Z | 265.499° W | 29.606° | 2025-10-17 05:59:39.628Z | 328.926° NNW |
| 4 mins | 2025-10-17 18:51:39.628Z | 337.436° NNW | 2025-10-17 18:53:39.628Z | 286.704° WNW | 25.356° | 2025-10-17 18:55:39.628Z | 237.561° WSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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