FLOCK 4BE 10, 60503
Orbit data source: Space-Track
FLOCK 4BE 10, 60503 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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60503 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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4BE 10
1 60503U 24149AM 25320.68404981 .00103852 00000-0 27543-2 0 9998
2 60503 97.3981 38.5500 0004471 296.6299 63.4488 15.37903854 69657Epoch: 2025-11-16T16:25Z
TLE epoch observation values (Epoch: 2025-11-16T16:25:01.903Z)
Latitude
0.00002°
Longitude
96.29676°
Altitude
454.059 km
Speed
7.641 km/s
True Right ascension
02h 34m 11s
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
05:43:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
452.303 km
Perigee altitude
446.198 km
Semi-major axis
6,827.387 km
Eccentricity
0.00045
Inclination
97.3981°
RAAN
38.55°
Arg. of periapsis
296.6299°
True anomaly
63.49464°
Mean anomaly
63.4488°
Eccentric anomaly
63.47172°
Mean motion
3.84735 °/min
Orbital period
93.57 mins
BSTAR
0.0027543
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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 10 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 | 2025-11-17 17:57:25.764Z | 22.837° NE | 2025-11-17 18:00:25.764Z | 92.646° ESE | 38.339° | 2025-11-17 18:03:25.764Z | 176.316° S |
| 4 mins | 2025-11-18 06:02:25.764Z | 230.59° WSW | 2025-11-18 06:03:25.764Z | 257.646° W | 22.869° | 2025-11-18 06:06:25.764Z | 320.83° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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