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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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, 0.1 m
Radar Cross Section
0.035 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 17
1 60492U 24149AA 25256.75911615 .00011056 00000-0 38883-3 0 9992
2 60492 97.4044 334.5318 0004571 157.9990 202.1447 15.29511763 59852Epoch: 2025-09-13T18:13Z
TLE epoch observation values (Epoch: 2025-09-13T18:13:07.635Z)
Latitude
-0.00005°
Longitude
68.26213°
Altitude
483.277 km
Speed
7.622 km/s
True Right ascension
22h 18m 07s
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
21:17:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.356 km
Perigee altitude
471.092 km
Semi-major axis
6,852.361 km
Eccentricity
0.00046
Inclination
97.4044°
RAAN
334.5318°
Arg. of periapsis
157.999°
True anomaly
202.12497°
Mean anomaly
202.1447°
Eccentric anomaly
202.13483°
Mean motion
3.82633 °/min
Orbital period
94.08 mins
BSTAR
0.00038883
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-14 05:20:22.217Z | 168.692° S | 2025-09-14 05:23:22.217Z | 334.385° NNW | 43.973° | 2025-09-14 05:26:22.217Z | 347.177° N |
| 5 mins | 2025-09-14 18:20:22.217Z | 0.561° NNE | 2025-09-14 18:22:22.217Z | 310.236° NW | 40.734° | 2025-09-14 18:25:22.217Z | 205.648° SW |
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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