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: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4BE 32
1 60497U 24149AF 26305.19231127 .00025143 00000-0 48124-3 0 9995
2 60497 97.3638 31.0553 0005122 134.5003 225.6667 15.48034540123483Epoch: 2026-11-01T04:36Z
TLE epoch observation values (Epoch: 2026-11-01T04:36:55.693Z)
Latitude
-0.00002°
Longitude
-78.66396°
Altitude
428.041 km
Speed
7.653 km/s
True Right ascension
02h 04m 13s
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
11:04:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
422.885 km
Perigee altitude
415.921 km
Semi-major axis
6,797.54 km
Eccentricity
0.00051
Inclination
97.3638°
RAAN
31.0553°
Arg. of periapsis
134.5003°
True anomaly
225.62474°
Mean anomaly
225.6667°
Eccentric anomaly
225.64572°
Mean motion
3.87271 °/min
Orbital period
92.96 mins
BSTAR
0.00048124
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-01 19:07:47.530Z | 353.48° N | 2026-11-01 19:10:47.530Z | 270.042° WNW | 37.106° | 2026-11-01 19:12:47.530Z | 221.66° SW |
| 5 mins | 2026-11-02 05:34:47.530Z | 137.51° SSE | 2026-11-02 05:36:47.530Z | 77.328° E | 40.713° | 2026-11-02 05:39:47.530Z | 3.7° NNE |
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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