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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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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4BE 29
1 60509U 24149AT 25289.44735516 .00019393 00000-0 60184-3 0 9998
2 60509 97.4037 8.2289 0004424 93.7888 266.3860 15.33421057 64921Epoch: 2025-10-16T10:44Z
TLE epoch observation values (Epoch: 2025-10-16T10:44:11.485Z)
Latitude
-0.00008°
Longitude
-178.02589°
Altitude
468.915 km
Speed
7.632 km/s
True Right ascension
00h 32m 54s
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
14:42:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.589 km
Perigee altitude
459.536 km
Semi-major axis
6,840.699 km
Eccentricity
0.00044
Inclination
97.4037°
RAAN
8.2289°
Arg. of periapsis
93.7888°
True anomaly
266.33541°
Mean anomaly
266.386°
Eccentric anomaly
266.3607°
Mean motion
3.83612 °/min
Orbital period
93.84 mins
BSTAR
0.00060184
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-17 05:39:23.187Z | 183.654° SSW | 2025-10-17 05:42:23.187Z | 278.442° WNW | 38.563° | 2025-10-17 05:45:23.187Z | 338.206° N |
| 4 mins | 2025-10-17 18:38:23.187Z | 335.808° NNW | 2025-10-17 18:39:23.187Z | 300.278° NW | 33.274° | 2025-10-17 18:42:23.187Z | 217.633° 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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