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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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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4BE 24
1 60505U 24149AP 26035.20189675 .00021260 00000-0 57564-3 0 9991
2 60505 97.3817 118.4824 0004661 53.2770 306.8902 15.37688293 81898Epoch: 2026-02-04T04:50Z
TLE epoch observation values (Epoch: 2026-02-04T04:50:43.879Z)
Latitude
-0.00003°
Longitude
-88.57229°
Altitude
454.151 km
Speed
7.641 km/s
True Right ascension
07h 53m 55s
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
12:25:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.071 km
Perigee altitude
446.706 km
Semi-major axis
6,828.025 km
Eccentricity
0.00047
Inclination
97.3817°
RAAN
118.4824°
Arg. of periapsis
53.277°
True anomaly
306.84747°
Mean anomaly
306.8902°
Eccentric anomaly
306.86884°
Mean motion
3.84681 °/min
Orbital period
93.58 mins
BSTAR
0.00057564
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-04 17:54:14.269Z | 32.352° NE | 2026-02-04 17:57:14.269Z | 113.277° SE | 30.672° | 2026-02-04 17:59:14.269Z | 161.284° S |
| 5 mins | 2026-02-05 05:58:14.269Z | 206.086° SW | 2026-02-05 06:00:14.269Z | 261.904° W | 28.903° | 2026-02-05 06:03:14.269Z | 328.086° NNW |
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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