FLOCK 4BE 34, 60495
Orbit data source: Space-Track
FLOCK 4BE 34, 60495 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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60495 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: 19 hours ago
TLE from 19 hours ago
0 FLOCK 4BE 34
1 60495U 24149AD 26129.18226036 .00012564 00000-0 31626-3 0 9991
2 60495 97.3775 213.2082 0004741 77.3130 282.8646 15.40048807 96322Epoch: 2026-05-09T04:22Z
TLE epoch observation values (Epoch: 2026-05-09T04:22:27.295Z)
Latitude
0.00002°
Longitude
-79.4089°
Altitude
448.364 km
Speed
7.644 km/s
True Right ascension
14h 12m 49s
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
07:44:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
446.137 km
Perigee altitude
439.669 km
Semi-major axis
6,821.04 km
Eccentricity
0.00047
Inclination
97.3775°
RAAN
213.2082°
Arg. of periapsis
77.313°
True anomaly
282.81163°
Mean anomaly
282.8646°
Eccentric anomaly
282.83812°
Mean motion
3.85272 °/min
Orbital period
93.44 mins
BSTAR
0.00031626
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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 34 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 | 2026-05-10 05:27:34.583Z | 153.888° SSE | 2026-05-10 05:29:34.583Z | 117.616° SE | 38.971° | 2026-05-10 05:32:34.583Z | 357.587° N |
| 5 mins | 2026-05-10 18:22:34.583Z | 20.873° NNE | 2026-05-10 18:24:34.583Z | 147.278° SSE | 42.511° | 2026-05-10 18:27:34.583Z | 186.991° 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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