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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4BE 32
1 60497U 24149AF 25310.19789630 .00024526 00000-0 77063-3 0 9995
2 60497 97.3945 27.9467 0004001 7.3904 352.7397 15.32978165 68061Epoch: 2025-11-06T04:44Z
TLE epoch observation values (Epoch: 2025-11-06T04:44:58.240Z)
Latitude
0.00004°
Longitude
-88.95563°
Altitude
467.323 km
Speed
7.634 km/s
True Right ascension
01h 51m 47s
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
07:38:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.618 km
Perigee altitude
461.143 km
Semi-major axis
6,842.018 km
Eccentricity
0.0004
Inclination
97.3945°
RAAN
27.9467°
Arg. of periapsis
7.3904°
True anomaly
352.7339°
Mean anomaly
352.7397°
Eccentric anomaly
352.7368°
Mean motion
3.83501 °/min
Orbital period
93.87 mins
BSTAR
0.00077063
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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 | 2025-11-06 17:50:35.643Z | 27.662° NE | 2025-11-06 17:53:35.643Z | 101.389° ESE | 34.577° | 2025-11-06 17:56:35.643Z | 171.07° S |
| 4 mins | 2025-11-07 05:57:35.643Z | 221.524° SW | 2025-11-07 05:58:35.643Z | 247.186° WSW | 24.673° | 2025-11-07 06:01:35.643Z | 319.806° NNW |
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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