FLOCK 4BE 17, 60492
Orbit data source: Space-Track
FLOCK 4BE 17, 60492 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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60492 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4BE 17
1 60492U 24149AA 26252.50858938 .00027859 00000-0 64819-3 0 9996
2 60492 97.3731 336.6619 0001689 332.2786 27.8371 15.42273156115249Epoch: 2026-09-09T12:12Z
TLE epoch observation values (Epoch: 2026-09-09T12:12:22.122Z)
Latitude
-0.00002°
Longitude
165.01009°
Altitude
441.505 km
Speed
7.648 km/s
True Right ascension
22h 26m 38s
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
12:35:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
437.488 km
Perigee altitude
435.186 km
Semi-major axis
6,814.474 km
Eccentricity
0.00017
Inclination
97.3731°
RAAN
336.6619°
Arg. of periapsis
332.2786°
True anomaly
27.84614°
Mean anomaly
27.8371°
Eccentric anomaly
27.84162°
Mean motion
3.85829 °/min
Orbital period
93.31 mins
BSTAR
0.00064819
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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 17 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 | 2026-09-10 05:28:22.564Z | 144.504° SSE | 2026-09-10 05:30:22.564Z | 95.314° ESE | 45.748° | 2026-09-10 05:33:22.564Z | 2.627° NNE |
| 4 mins | 2026-09-10 18:22:22.564Z | 34.33° NE | 2026-09-10 18:23:22.564Z | 64.095° ENE | 48.312° | 2026-09-10 18:26:22.564Z | 175.584° 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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