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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4BE 6
1 60516U 24149BA 25290.78639617 .00023570 00000-0 78873-3 0 9996
2 60516 97.4026 8.6805 0005318 94.3307 265.8542 15.30955988 65071Epoch: 2025-10-17T18:52Z
TLE epoch observation values (Epoch: 2025-10-17T18:52:24.629Z)
Latitude
0.00002°
Longitude
59.05111°
Altitude
476.329 km
Speed
7.627 km/s
True Right ascension
00h 34m 43s
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
21:00:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.552 km
Perigee altitude
466.268 km
Semi-major axis
6,848.047 km
Eccentricity
0.00053
Inclination
97.4026°
RAAN
8.6805°
Arg. of periapsis
94.3307°
True anomaly
265.79342°
Mean anomaly
265.8542°
Eccentric anomaly
265.82381°
Mean motion
3.82995 °/min
Orbital period
94 mins
BSTAR
0.00078873
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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 | 2025-10-18 04:26:33.735Z | 103.707° ESE | 2025-10-18 04:28:33.735Z | 65.942° ENE | 15.64° | 2025-10-18 04:30:33.735Z | 29.958° NE |
| 4 mins | 2025-10-18 05:59:33.735Z | 217.402° SW | 2025-10-18 06:01:33.735Z | 267.273° W | 23.895° | 2025-10-18 06:03:33.735Z | 313.021° NW |
| 4 mins | 2025-10-18 18:58:33.735Z | 322.948° NNW | 2025-10-18 18:59:33.735Z | 301.094° NW | 19.407° | 2025-10-18 19:02:33.735Z | 240.649° 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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