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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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: 21 hours ago
TLE from 21 hours ago
0 FLOCK 4BE 6
1 60516U 24149BA 25338.66215816 .00032048 00000-0 10014-2 0 9999
2 60516 97.3988 56.5073 0002724 272.3546 87.7384 15.33103229 72403Epoch: 2025-12-04T15:53Z
TLE epoch observation values (Epoch: 2025-12-04T15:53:30.465Z)
Latitude
-0.00003°
Longitude
104.41498°
Altitude
469.595 km
Speed
7.631 km/s
True Right ascension
03h 46m 01s
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
11:17:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.372 km
Perigee altitude
461.645 km
Semi-major axis
6,841.645 km
Eccentricity
0.00027
Inclination
97.3988°
RAAN
56.5073°
Arg. of periapsis
272.3546°
True anomaly
87.76959°
Mean anomaly
87.7384°
Eccentric anomaly
87.754°
Mean motion
3.83533 °/min
Orbital period
93.86 mins
BSTAR
0.0010014
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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 | 2025-12-05 17:32:09.469Z | 53.053° ENE | 2025-12-05 17:34:09.469Z | 98.224° ESE | 20.919° | 2025-12-05 17:36:09.469Z | 141.11° SSE |
| 5 mins | 2025-12-06 05:37:09.469Z | 183.876° SSW | 2025-12-06 05:39:09.469Z | 229.805° WSW | 39.095° | 2025-12-06 05:42:09.469Z | 336.877° NNW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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