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: 1 day ago
TLE from 1 day ago
0 FLOCK 4BE 13
1 60512U 24149AW 26174.19117784 .00011933 00000-0 28161-3 0 9990
2 60512 97.3715 258.6653 0003274 231.4286 128.6668 15.42025241103293Epoch: 2026-06-23T04:35Z
TLE epoch observation values (Epoch: 2026-06-23T04:35:17.765Z)
Latitude
-0.00003°
Longitude
-81.525°
Altitude
444.649 km
Speed
7.645 km/s
True Right ascension
17h 14m 39s
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
21:47:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
439.299 km
Perigee altitude
434.837 km
Semi-major axis
6,815.205 km
Eccentricity
0.00033
Inclination
97.3715°
RAAN
258.6653°
Arg. of periapsis
231.4286°
True anomaly
128.69609°
Mean anomaly
128.6668°
Eccentric anomaly
128.68144°
Mean motion
3.85767 °/min
Orbital period
93.32 mins
BSTAR
0.00028161
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-24 18:31:37.308Z | 12.37° NNE | 2026-06-24 18:34:37.308Z | 189.644° SSW | 42.234° | 2026-06-24 18:36:37.308Z | 192.214° SSW |
| 4 mins | 2026-06-25 05:01:37.308Z | 105.973° ESE | 2026-06-25 05:02:37.308Z | 82.565° E | 20.188° | 2026-06-25 05:05:37.308Z | 18.773° NNE |
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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