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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60512 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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4BE 13
1 60512U 24149AW 25289.11872022 .00019250 00000-0 61296-3 0 9997
2 60512 97.3951 7.2817 0005679 71.7953 288.3907 15.32593594 64861Epoch: 2025-10-16T02:50Z
TLE epoch observation values (Epoch: 2025-10-16T02:50:57.427Z)
Latitude
0.00003°
Longitude
-60.34061°
Altitude
469.96 km
Speed
7.632 km/s
True Right ascension
00h 29m 07s
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
14:41:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.912 km
Perigee altitude
461.14 km
Semi-major axis
6,843.163 km
Eccentricity
0.00057
Inclination
97.3951°
RAAN
7.2817°
Arg. of periapsis
71.7953°
True anomaly
288.32893°
Mean anomaly
288.3907°
Eccentric anomaly
288.35982°
Mean motion
3.83405 °/min
Orbital period
93.9 mins
BSTAR
0.00061296
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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 | 2025-10-17 05:36:41.677Z | 182.824° SSW | 2025-10-17 05:39:41.677Z | 266.879° W | 39.11° | 2025-10-17 05:42:41.677Z | 337.652° N |
| 5 mins | 2025-10-17 18:35:41.677Z | 345.088° N | 2025-10-17 18:37:41.677Z | 277.135° WNW | 33.412° | 2025-10-17 18:40:41.677Z | 215.226° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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