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: 22 hours ago
TLE from 22 hours ago
0 FLOCK 4BE 32
1 60497U 24149AF 26171.04293401 .00015606 00000-0 36492-3 0 9991
2 60497 97.3718 255.0009 0002674 242.2970 117.8006 15.42240995102770Epoch: 2026-06-20T01:01Z
TLE epoch observation values (Epoch: 2026-06-20T01:01:49.498Z)
Latitude
-0.00004°
Longitude
-28.71857°
Altitude
443.469 km
Speed
7.645 km/s
True Right ascension
17h 00m 00s
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
10:18:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
438.254 km
Perigee altitude
434.609 km
Semi-major axis
6,814.569 km
Eccentricity
0.00027
Inclination
97.3718°
RAAN
255.0009°
Arg. of periapsis
242.297°
True anomaly
117.8277°
Mean anomaly
117.8006°
Eccentric anomaly
117.81415°
Mean motion
3.85821 °/min
Orbital period
93.31 mins
BSTAR
0.00036492
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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 | 2026-06-21 05:11:42.712Z | 135.686° SSE | 2026-06-21 05:14:42.712Z | 58.851° ENE | 28.032° | 2026-06-21 05:16:42.712Z | 13.387° NNE |
| 4 mins | 2026-06-21 18:05:42.712Z | 42.981° NE | 2026-06-21 18:07:42.712Z | 110.055° ESE | 30.379° | 2026-06-21 18:09:42.712Z | 160.502° 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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