FLOCK 4BE 11, 60501
Orbit data source: Space-Track
FLOCK 4BE 11, 60501 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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60501 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, 0.1 m
Radar Cross Section
0.035 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 11
1 60501U 24149AK 25260.19983089 .00012700 00000-0 42693-3 0 9991
2 60501 97.3974 338.0781 0005996 159.7514 200.3966 15.30938196 60416Epoch: 2025-09-17T04:47Z
TLE epoch observation values (Epoch: 2025-09-17T04:47:45.388Z)
Latitude
-0.00005°
Longitude
-90.24021°
Altitude
479.969 km
Speed
7.623 km/s
True Right ascension
22h 32m 18s
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
15:01:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.069 km
Perigee altitude
465.857 km
Semi-major axis
6,848.1 km
Eccentricity
0.0006
Inclination
97.3974°
RAAN
338.0781°
Arg. of periapsis
159.7514°
True anomaly
200.37267°
Mean anomaly
200.3966°
Eccentric anomaly
200.38463°
Mean motion
3.82991 °/min
Orbital period
94 mins
BSTAR
0.00042693
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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 11 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 | 2025-09-18 04:28:37.038Z | 110.755° ESE | 2025-09-18 04:30:37.038Z | 73.699° E | 17.404° | 2025-09-18 04:32:37.038Z | 33.08° NE |
| 4 mins | 2025-09-18 06:02:37.038Z | 232.611° WSW | 2025-09-18 06:03:37.038Z | 257.294° W | 21.641° | 2025-09-18 06:06:37.038Z | 318.18° NNW |
| 4 mins | 2025-09-18 17:27:37.038Z | 56.389° ENE | 2025-09-18 17:29:37.038Z | 103.469° ESE | 20.606° | 2025-09-18 17:31:37.038Z | 143.456° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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