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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FLOCK 4BE 10 radio frequencies
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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, 0.1 m
Radar Cross Section
0.035 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 10
1 60503U 24149AM 25261.80320024 .00010952 00000-0 38208-3 0 9990
2 60503 97.4040 339.6495 0004754 152.2032 207.9464 15.29777584 60636Epoch: 2025-09-18T19:16Z
TLE epoch observation values (Epoch: 2025-09-18T19:16:36.5Z)
Latitude
0.00003°
Longitude
52.53786°
Altitude
482.46 km
Speed
7.623 km/s
True Right ascension
22h 38m 35s
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
23:30:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.687 km
Perigee altitude
470.172 km
Semi-major axis
6,851.566 km
Eccentricity
0.00048
Inclination
97.404°
RAAN
339.6495°
Arg. of periapsis
152.2032°
True anomaly
207.92088°
Mean anomaly
207.9464°
Eccentric anomaly
207.93364°
Mean motion
3.827 °/min
Orbital period
94.07 mins
BSTAR
0.00038208
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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 | 2025-09-19 17:48:44.229Z | 25.496° NE | 2025-09-19 17:51:44.229Z | 85.055° E | 34.824° | 2025-09-19 17:54:44.229Z | 170.001° S |
| 4 mins | 2025-09-20 05:57:44.229Z | 227.596° WSW | 2025-09-20 05:58:44.229Z | 254.149° W | 24.269° | 2025-09-20 06:01:44.229Z | 320.225° 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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