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
Partially 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 35
1 60558U 24149CU 26084.18590431 .00094747 00000-0 18739-2 0 9996
2 60558 97.3758 167.6829 0006154 217.2288 142.8536 15.46744979 89394Epoch: 2026-03-25T04:27Z
TLE epoch observation values (Epoch: 2026-03-25T04:27:42.132Z)
Latitude
0.00001°
Longitude
-81.89548°
Altitude
432.722 km
Speed
7.65 km/s
True Right ascension
11h 10m 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
23:33:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
427.37 km
Perigee altitude
418.999 km
Semi-major axis
6,801.322 km
Eccentricity
0.00062
Inclination
97.3758°
RAAN
167.6829°
Arg. of periapsis
217.2288°
True anomaly
142.89616°
Mean anomaly
142.8536°
Eccentric anomaly
142.87488°
Mean motion
3.86949 °/min
Orbital period
93.04 mins
BSTAR
0.0018739
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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 | 2026-03-25 18:59:21.885Z | 342.435° N | 2026-03-25 19:01:21.885Z | 301.543° NW | 22.469° | 2026-03-25 19:04:21.885Z | 232.117° WSW |
| 4 mins | 2026-03-26 05:27:21.885Z | 151.048° SSE | 2026-03-26 05:28:21.885Z | 116.144° SE | 41.857° | 2026-03-26 05:31:21.885Z | 354.221° N |
| 4 mins | 2026-03-26 18:17:21.885Z | 18.827° NNE | 2026-03-26 18:19:21.885Z | 73.323° E | 43.196° | 2026-03-26 18:21:21.885Z | 182.652° SSW |
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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