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, 1.0 m
Radar Cross Section
0.072 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 FLOCK 4BE 17
1 60492U 24149AA 25286.90739752 .00018591 00000-0 62701-3 0 9999
2 60492 97.4013 4.5728 0004327 78.0023 282.1703 15.30755353 64469Epoch: 2025-10-13T21:46Z
TLE epoch observation values (Epoch: 2025-10-13T21:46:39.145Z)
Latitude
-0.00002°
Longitude
15.20626°
Altitude
476.039 km
Speed
7.628 km/s
True Right ascension
00h 18m 17s
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
06:49:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.472 km
Perigee altitude
467.545 km
Semi-major axis
6,848.646 km
Eccentricity
0.00043
Inclination
97.4013°
RAAN
4.5728°
Arg. of periapsis
78.0023°
True anomaly
282.12183°
Mean anomaly
282.1703°
Eccentric anomaly
282.14606°
Mean motion
3.82945 °/min
Orbital period
94.01 mins
BSTAR
0.00062701
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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 | 2025-10-14 18:44:22.215Z | 338.942° N | 2025-10-14 18:46:22.215Z | 288.266° WNW | 26.547° | 2025-10-14 18:49:22.215Z | 226.378° WSW |
| 5 mins | 2025-10-15 05:17:22.215Z | 162.862° S | 2025-10-15 05:19:22.215Z | 146.355° SSE | 42.314° | 2025-10-15 05:22:22.215Z | 351.022° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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