FLOCK 4BE 24, 60505
Orbit data source: Space-Track
FLOCK 4BE 24, 60505 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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60505 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: 15 hours ago
TLE from 15 hours ago
0 FLOCK 4BE 24
1 60505U 24149AP 26171.21694257 .00016897 00000-0 38285-3 0 9999
2 60505 97.3712 255.6671 0002914 257.1798 102.9124 15.43167776102834Epoch: 2026-06-20T05:12Z
TLE epoch observation values (Epoch: 2026-06-20T05:12:23.838Z)
Latitude
-0.00002°
Longitude
-90.86696°
Altitude
440.334 km
Speed
7.647 km/s
True Right ascension
17h 02m 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
07:24:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
435.686 km
Perigee altitude
431.716 km
Semi-major axis
6,811.838 km
Eccentricity
0.00029
Inclination
97.3712°
RAAN
255.6671°
Arg. of periapsis
257.1798°
True anomaly
102.94494°
Mean anomaly
102.9124°
Eccentric anomaly
102.92867°
Mean motion
3.86053 °/min
Orbital period
93.25 mins
BSTAR
0.00038285
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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 24 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 | 2026-06-21 06:15:20.265Z | 224.695° SW | 2026-06-21 06:16:20.265Z | 255.096° W | 25.788° | 2026-06-21 06:19:20.265Z | 324.167° NNW |
| 4 mins | 2026-06-21 19:07:20.265Z | 335.008° NNW | 2026-06-21 19:09:20.265Z | 280.94° WNW | 24.275° | 2026-06-21 19:11:20.265Z | 235.141° WSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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