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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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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4BE 35
1 60558U 24149CU 25290.76676170 .00024022 00000-0 80069-3 0 9998
2 60558 97.4005 8.6291 0004341 90.4210 269.7528 15.31083327 65075Epoch: 2025-10-17T18:24Z
TLE epoch observation values (Epoch: 2025-10-17T18:24:08.210Z)
Latitude
-0.00011°
Longitude
66.08749°
Altitude
475.699 km
Speed
7.628 km/s
True Right ascension
00h 34m 30s
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
20:59:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.502 km
Perigee altitude
466.557 km
Semi-major axis
6,847.667 km
Eccentricity
0.00043
Inclination
97.4005°
RAAN
8.6291°
Arg. of periapsis
90.421°
True anomaly
269.70306°
Mean anomaly
269.7528°
Eccentric anomaly
269.72793°
Mean motion
3.83027 °/min
Orbital period
93.99 mins
BSTAR
0.00080069
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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 | 2025-10-18 05:30:49.191Z | 178.792° S | 2025-10-18 05:33:49.191Z | 306.583° NW | 39.761° | 2025-10-18 05:35:49.191Z | 339.206° N |
| 5 mins | 2025-10-18 18:29:49.191Z | 353.418° N | 2025-10-18 18:31:49.191Z | 298.867° NW | 36.424° | 2025-10-18 18:34:49.191Z | 213.127° SW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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