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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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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4BE 32
1 60497U 24149AF 25290.67535834 .00025921 00000-0 83702-3 0 9997
2 60497 97.3959 8.4432 0005387 70.4207 289.7615 15.32085960 65079Epoch: 2025-10-17T16:12Z
TLE epoch observation values (Epoch: 2025-10-17T16:12:30.960Z)
Latitude
-0.00012°
Longitude
98.89689°
Altitude
471.451 km
Speed
7.631 km/s
True Right ascension
00h 33m 46s
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
16:38:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.226 km
Perigee altitude
462.852 km
Semi-major axis
6,844.676 km
Eccentricity
0.00054
Inclination
97.3959°
RAAN
8.4432°
Arg. of periapsis
70.4207°
True anomaly
289.70339°
Mean anomaly
289.7615°
Eccentric anomaly
289.73245°
Mean motion
3.83278 °/min
Orbital period
93.93 mins
BSTAR
0.00083702
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-18 04:52:47.283Z | 138.448° SSE | 2025-10-18 04:55:47.283Z | 71.845° E | 29.828° | 2025-10-18 04:58:47.283Z | 7.314° NNE |
| 5 mins | 2025-10-18 17:51:47.283Z | 33.361° NE | 2025-10-18 17:53:47.283Z | 92.316° ESE | 35.458° | 2025-10-18 17:56:47.283Z | 171.484° S |
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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