FLOCK 4BE 35, 60558
Orbit data source: Space-Track
FLOCK 4BE 35, 60558 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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60558 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Non-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: 10 hours ago
TLE from 10 hours ago
0 FLOCK 4BE 35
1 60558U 24149CU 26144.84412657 .00148386 00000-0 17184-2 0 9991
2 60558 97.3694 230.0991 0002479 255.9992 104.0990 15.61335382 98817Epoch: 2026-05-24T20:15Z
TLE epoch observation values (Epoch: 2026-05-24T20:15:32.535Z)
Latitude
-0.00003°
Longitude
43.7731°
Altitude
387.355 km
Speed
7.677 km/s
True Right ascension
15h 20m 23s
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
15:28:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
382.384 km
Perigee altitude
379.033 km
Semi-major axis
6,758.845 km
Eccentricity
0.00025
Inclination
97.3694°
RAAN
230.0991°
Arg. of periapsis
255.9992°
True anomaly
104.12655°
Mean anomaly
104.099°
Eccentric anomaly
104.11277°
Mean motion
3.90602 °/min
Orbital period
92.17 mins
BSTAR
0.0017184
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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 35 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 | 2026-05-25 18:20:47.863Z | 23.036° NE | 2026-05-25 18:23:47.863Z | 133.376° SE | 36.623° | 2026-05-25 18:25:47.863Z | 176.513° S |
| 4 mins | 2026-05-26 06:13:47.863Z | 208.225° SW | 2026-05-26 06:15:47.863Z | 266.03° W | 25.441° | 2026-05-26 06:17:47.863Z | 318.791° 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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