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: 22 hours ago
TLE from 22 hours ago
0 FLOCK 4BE 17
1 60492U 24149AA 26042.18232667 .00016160 00000-0 46777-3 0 9998
2 60492 97.3867 124.8922 0002677 11.0011 349.1290 15.35669785 82897Epoch: 2026-02-11T04:22Z
TLE epoch observation values (Epoch: 2026-02-11T04:22:33.024Z)
Latitude
-0.00008°
Longitude
-81.9975°
Altitude
460.246 km
Speed
7.638 km/s
True Right ascension
08h 19m 34s
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
04:44:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.705 km
Perigee altitude
454.046 km
Semi-major axis
6,834.013 km
Eccentricity
0.00027
Inclination
97.3867°
RAAN
124.8922°
Arg. of periapsis
11.0011°
True anomaly
349.12321°
Mean anomaly
349.129°
Eccentric anomaly
349.12611°
Mean motion
3.84175 °/min
Orbital period
93.71 mins
BSTAR
0.00046777
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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 | 2026-02-12 05:31:04.529Z | 171.19° S | 2026-02-12 05:34:04.529Z | 215.25° SW | 43.994° | 2026-02-12 05:37:04.529Z | 344.756° N |
| 4 mins | 2026-02-12 18:29:04.529Z | 356.146° N | 2026-02-12 18:31:04.529Z | 248.38° W | 39.922° | 2026-02-12 18:33:04.529Z | 206.776° 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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