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: 16 hours ago
TLE from 16 hours ago
0 FLOCK 4BE 24
1 60505U 24149AP 25303.16621784 .00024669 00000-0 76832-3 0 9990
2 60505 97.3945 21.1777 0004774 41.7999 318.3607 15.33256181 67007Epoch: 2025-10-30T03:59Z
TLE epoch observation values (Epoch: 2025-10-30T03:59:21.221Z)
Latitude
-0.00004°
Longitude
-77.38962°
Altitude
466.772 km
Speed
7.634 km/s
True Right ascension
01h 24m 42s
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
15:35:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.319 km
Perigee altitude
459.787 km
Semi-major axis
6,841.19 km
Eccentricity
0.00048
Inclination
97.3945°
RAAN
21.1777°
Arg. of periapsis
41.7999°
True anomaly
318.32433°
Mean anomaly
318.3607°
Eccentric anomaly
318.34252°
Mean motion
3.83571 °/min
Orbital period
93.85 mins
BSTAR
0.00076832
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-31 05:10:40.373Z | 154.238° SSE | 2025-10-31 05:13:40.373Z | 68.915° E | 40.782° | 2025-10-31 05:16:40.373Z | 356.686° N |
| 5 mins | 2025-10-31 18:09:40.373Z | 18.717° NNE | 2025-10-31 18:11:40.373Z | 168.009° S | 42.014° | 2025-10-31 18:14:40.373Z | 189.12° SSW |
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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