FLOCK 4BE 6, 60516
Orbit data source: Space-Track
FLOCK 4BE 6, 60516 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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60516 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: 1 day ago
TLE from 1 day ago
0 FLOCK 4BE 6
1 60516U 24149BA 26296.97336952 .00017666 00000-0 38856-3 0 9996
2 60516 97.3727 21.9107 0003787 170.0932 190.0392 15.44039314122117Epoch: 2026-10-23T23:21Z
TLE epoch observation values (Epoch: 2026-10-23T23:21:39.126Z)
Latitude
0.00002°
Longitude
-0.88856°
Altitude
439.867 km
Speed
7.647 km/s
True Right ascension
01h 27m 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
02:19:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
433.713 km
Perigee altitude
428.556 km
Semi-major axis
6,809.272 km
Eccentricity
0.00038
Inclination
97.3727°
RAAN
21.9107°
Arg. of periapsis
170.0932°
True anomaly
190.03164°
Mean anomaly
190.0392°
Eccentric anomaly
190.03542°
Mean motion
3.86271 °/min
Orbital period
93.2 mins
BSTAR
0.00038856
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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 6 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 | 2026-10-25 17:56:02.677Z | 55.647° ENE | 2026-10-25 17:58:02.677Z | 99.732° ESE | 19.06° | 2026-10-25 18:00:02.677Z | 139.922° SSE |
| 5 mins | 2026-10-26 05:56:02.677Z | 173.146° S | 2026-10-26 05:58:02.677Z | 216.28° SW | 74.133° | 2026-10-26 06:01:02.677Z | 344.713° N |
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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