FLOCK 4BE 13, 60512
Orbit data source: Space-Track
FLOCK 4BE 13, 60512 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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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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4BE 13
1 60512U 24149AW 26129.78763213 .00010397 00000-0 25520-3 0 9998
2 60512 97.3713 213.8327 0004946 62.7608 297.4142 15.40865058 96459Epoch: 2026-05-09T18:54Z
TLE epoch observation values (Epoch: 2026-05-09T18:54:11.416Z)
Latitude
0.00001°
Longitude
62.68508°
Altitude
445.122 km
Speed
7.646 km/s
True Right ascension
14h 15m 19s
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
09:50:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
443.864 km
Perigee altitude
437.119 km
Semi-major axis
6,818.629 km
Eccentricity
0.00049
Inclination
97.3713°
RAAN
213.8327°
Arg. of periapsis
62.7608°
True anomaly
297.36387°
Mean anomaly
297.4142°
Eccentric anomaly
297.38904°
Mean motion
3.85476 °/min
Orbital period
93.39 mins
BSTAR
0.0002552
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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 13 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-10 05:56:00.747Z | 186.332° SSW | 2026-05-10 05:59:00.747Z | 258.076° W | 35.661° | 2026-05-10 06:02:00.747Z | 334.305° NNW |
| 4 mins | 2026-05-10 18:51:00.747Z | 345.263° N | 2026-05-10 18:53:00.747Z | 277.698° WNW | 32.612° | 2026-05-10 18:55:00.747Z | 222.925° SW |
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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