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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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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4BE 5
1 60559U 24149CV 26111.80157680 .00014985 00000-0 39461-3 0 9994
2 60559 97.3836 195.3317 0004687 134.1867 225.9764 15.38622783 93605Epoch: 2026-04-21T19:14Z
TLE epoch observation values (Epoch: 2026-04-21T19:14:16.235Z)
Latitude
-0.00003°
Longitude
56.89192°
Altitude
455.523 km
Speed
7.638 km/s
True Right ascension
13h 01m 19s
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
18:58:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.32 km
Perigee altitude
443.922 km
Semi-major axis
6,825.258 km
Eccentricity
0.00047
Inclination
97.3836°
RAAN
195.3317°
Arg. of periapsis
134.1867°
True anomaly
225.9378°
Mean anomaly
225.9764°
Eccentric anomaly
225.9571°
Mean motion
3.84915 °/min
Orbital period
93.53 mins
BSTAR
0.00039461
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-22 17:39:41.617Z | 48.502° ENE | 2026-04-22 17:41:41.617Z | 87.051° E | 18.585° | 2026-04-22 17:43:41.617Z | 132.73° SE |
| 5 mins | 2026-04-23 05:42:41.617Z | 177.378° S | 2026-04-23 05:44:41.617Z | 223.32° SW | 42.314° | 2026-04-23 05:47:41.617Z | 341.827° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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