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: 14 hours ago
TLE from 14 hours ago
0 FLOCK 4BE 5
1 60559U 24149CV 26196.15009307 .00009250 00000-0 22602-3 0 9995
2 60559 97.3845 280.4332 0004055 171.5004 188.6312 15.41042056106584Epoch: 2026-07-15T03:36Z
TLE epoch observation values (Epoch: 2026-07-15T03:36:08.041Z)
Latitude
-0.00001°
Longitude
-66.61034°
Altitude
448.887 km
Speed
7.641 km/s
True Right ascension
18h 41m 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
05:48:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
442.734 km
Perigee altitude
437.205 km
Semi-major axis
6,818.106 km
Eccentricity
0.00041
Inclination
97.3845°
RAAN
280.4332°
Arg. of periapsis
171.5004°
True anomaly
188.62423°
Mean anomaly
188.6312°
Eccentric anomaly
188.62771°
Mean motion
3.85521 °/min
Orbital period
93.38 mins
BSTAR
0.00022602
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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 | 2026-07-15 18:11:42.836Z | 31.67° NE | 2026-07-15 18:13:42.836Z | 77.672° E | 32.592° | 2026-07-15 18:16:42.836Z | 168.173° S |
| 4 mins | 2026-07-16 06:14:42.836Z | 224.273° SW | 2026-07-16 06:15:42.836Z | 256.161° W | 27.004° | 2026-07-16 06:18:42.836Z | 325.347° NNW |
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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