FLOCK 4BE 32, 60497
Orbit data source: Space-Track
FLOCK 4BE 32, 60497 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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60497 intel report (Beta)
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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: 14 hours ago
TLE from 14 hours ago
0 FLOCK 4BE 32
1 60497U 24149AF 26219.74418939 .00011509 00000-0 25533-3 0 9998
2 60497 97.3698 304.2852 0005088 97.4608 262.7218 15.43879012110289Epoch: 2026-08-07T17:51Z
TLE epoch observation values (Epoch: 2026-08-07T17:51:37.963Z)
Latitude
-0.00005°
Longitude
80.11153°
Altitude
438.239 km
Speed
7.649 km/s
True Right ascension
20h 17m 08s
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
21:50:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
435.071 km
Perigee altitude
428.142 km
Semi-major axis
6,809.743 km
Eccentricity
0.00051
Inclination
97.3698°
RAAN
304.2852°
Arg. of periapsis
97.4608°
True anomaly
262.66397°
Mean anomaly
262.7218°
Eccentric anomaly
262.69288°
Mean motion
3.86231 °/min
Orbital period
93.21 mins
BSTAR
0.00025533
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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 32 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 | 2026-08-08 17:46:11.232Z | 55.417° ENE | 2026-08-08 17:48:11.232Z | 95.996° ESE | 16.331° | 2026-08-08 17:50:11.232Z | 135.501° SSE |
| 4 mins | 2026-08-09 05:47:11.232Z | 168.871° S | 2026-08-09 05:48:11.232Z | 171.925° S | 41.628° | 2026-08-09 05:51:11.232Z | 347.34° N |
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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