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
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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4BE 17
1 60492U 24149AA 26171.21006281 .00012363 00000-0 31331-3 0 9997
2 60492 97.3770 254.6033 0002378 220.8171 139.2897 15.39855558102725Epoch: 2026-06-20T05:02Z
TLE epoch observation values (Epoch: 2026-06-20T05:02:29.426Z)
Latitude
-0.00006°
Longitude
-89.44726°
Altitude
450.885 km
Speed
7.641 km/s
True Right ascension
16h 58m 24s
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
08:43:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
445.096 km
Perigee altitude
441.852 km
Semi-major axis
6,821.611 km
Eccentricity
0.00024
Inclination
97.377°
RAAN
254.6033°
Arg. of periapsis
220.8171°
True anomaly
139.30747°
Mean anomaly
139.2897°
Eccentric anomaly
139.29859°
Mean motion
3.85223 °/min
Orbital period
93.45 mins
BSTAR
0.00031331
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 06:08:00.857Z | 209.421° SW | 2026-06-21 06:10:00.857Z | 267.153° W | 27.845° | 2026-06-21 06:12:00.857Z | 318.488° NNW |
| 4 mins | 2026-06-21 19:03:00.857Z | 322.238° NNW | 2026-06-21 19:04:00.857Z | 292.055° WNW | 25.186° | 2026-06-21 19:07:00.857Z | 227.526° WSW |
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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