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: 18 hours ago
TLE from 18 hours ago
0 FLOCK 4BE 35
1 60558U 24149CU 26206.24401755 .00252793 00000-0 13629-2 0 9999
2 60558 97.3662 294.7097 0003773 195.3574 164.7579 15.79469759108449Epoch: 2026-07-25T05:51Z
TLE epoch observation values (Epoch: 2026-07-25T05:51:23.116Z)
Latitude
-0.00005°
Longitude
-96.09569°
Altitude
337.557 km
Speed
7.705 km/s
True Right ascension
19h 38m 50s
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
13:07:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
331.358 km
Perigee altitude
326.297 km
Semi-major axis
6,706.964 km
Eccentricity
0.00038
Inclination
97.3662°
RAAN
294.7097°
Arg. of periapsis
195.3574°
True anomaly
164.76926°
Mean anomaly
164.7579°
Eccentric anomaly
164.76358°
Mean motion
3.95143 °/min
Orbital period
91.11 mins
BSTAR
0.0013629
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-07-26 06:19:17.982Z | 198.525° SSW | 2026-07-26 06:21:17.982Z | 286.874° WNW | 30.338° | 2026-07-26 06:23:17.982Z | 331.654° NNW |
| 4 mins | 2026-07-26 18:54:17.982Z | 6.987° NNE | 2026-07-26 18:55:17.982Z | 355.001° N | 39.792° | 2026-07-26 18:58:17.982Z | 196.319° 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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