FLOCK 4BE 5, 60559
Orbit data source: Space-Track
FLOCK 4BE 5, 60559 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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60559 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 5
1 60559U 24149CV 25344.16034994 .00024333 00000-0 75965-3 0 9999
2 60559 97.4014 62.1474 0002569 242.4186 117.6795 15.33190178 73245Epoch: 2025-12-10T03:50Z
TLE epoch observation values (Epoch: 2025-12-10T03:50:54.234Z)
Latitude
-0.0001°
Longitude
-74.71323°
Altitude
470.227 km
Speed
7.631 km/s
True Right ascension
04h 08m 35s
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
16:19:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.007 km
Perigee altitude
461.492 km
Semi-major axis
6,841.387 km
Eccentricity
0.00026
Inclination
97.4014°
RAAN
62.1474°
Arg. of periapsis
242.4186°
True anomaly
117.70557°
Mean anomaly
117.6795°
Eccentric anomaly
117.69253°
Mean motion
3.83554 °/min
Orbital period
93.86 mins
BSTAR
0.00075965
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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 5 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 | 2025-12-10 18:30:27.796Z | 358.082° N | 2025-12-10 18:33:27.796Z | 253.574° W | 36.617° | 2025-12-10 18:35:27.796Z | 212.234° SW |
| 5 mins | 2025-12-11 05:03:27.796Z | 134.265° SE | 2025-12-11 05:05:27.796Z | 69.181° E | 33.707° | 2025-12-11 05:08:27.796Z | 3.532° NNE |
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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