FLOCK 4BE 29, 60509
Orbit data source: Space-Track
FLOCK 4BE 29, 60509 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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60509 intel report (Beta)
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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: 22 hours ago
TLE from 22 hours ago
0 FLOCK 4BE 29
1 60509U 24149AT 26297.17356463 .00048464 00000-0 80772-3 0 9994
2 60509 97.3762 25.5973 0002214 218.8449 141.2645 15.51851491122369Epoch: 2026-10-24T04:09Z
TLE epoch observation values (Epoch: 2026-10-24T04:09:55.984Z)
Latitude
0.00005°
Longitude
-69.46953°
Altitude
415.628 km
Speed
7.661 km/s
True Right ascension
01h 42m 23s
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
21:32:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
409.745 km
Perigee altitude
406.74 km
Semi-major axis
6,786.38 km
Eccentricity
0.00022
Inclination
97.3762°
RAAN
25.5973°
Arg. of periapsis
218.8449°
True anomaly
141.28037°
Mean anomaly
141.2645°
Eccentric anomaly
141.27244°
Mean motion
3.88227 °/min
Orbital period
92.73 mins
BSTAR
0.00080772
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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 29 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 | 2026-10-25 06:37:03.890Z | 218.74° SW | 2026-10-25 06:38:03.890Z | 247.075° WSW | 28.059° | 2026-10-25 06:41:03.890Z | 323.224° NNW |
| 4 mins | 2026-10-25 19:25:03.890Z | 338.207° N | 2026-10-25 19:27:03.890Z | 276.762° WNW | 30.097° | 2026-10-25 19:29:03.890Z | 229.033° WSW |
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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