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: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4BE 29
1 60509U 24149AT 26199.79061455 .00025598 00000-0 53151-3 0 9991
2 60509 97.3804 286.1681 0003838 167.5223 192.6121 15.45666248107291Epoch: 2026-07-18T18:58Z
TLE epoch observation values (Epoch: 2026-07-18T18:58:29.097Z)
Latitude
-0.00008°
Longitude
64.94857°
Altitude
435.097 km
Speed
7.649 km/s
True Right ascension
19h 04m 40s
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
18:30:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
428.963 km
Perigee altitude
423.74 km
Semi-major axis
6,804.489 km
Eccentricity
0.00038
Inclination
97.3804°
RAAN
286.1681°
Arg. of periapsis
167.5223°
True anomaly
192.6025°
Mean anomaly
192.6121°
Eccentric anomaly
192.6073°
Mean motion
3.86678 °/min
Orbital period
93.1 mins
BSTAR
0.00053151
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-19 05:58:51.908Z | 176.423° S | 2026-07-19 06:01:51.908Z | 311.542° NW | 40.035° | 2026-07-19 06:03:51.908Z | 340.958° N |
| 5 mins | 2026-07-19 18:50:51.908Z | 1.141° NNE | 2026-07-19 18:52:51.908Z | 284.425° WNW | 41.992° | 2026-07-19 18:55:51.908Z | 202.615° SW |
| 4 mins | 2026-07-20 05:18:51.908Z | 112.191° ESE | 2026-07-20 05:19:51.908Z | 84.872° E | 24.173° | 2026-07-20 05:22:51.908Z | 13.889° 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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