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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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: 15 hours ago
TLE from 15 hours ago
0 FLOCK 4BE 34
1 60495U 24149AD 25296.65787781 .00019011 00000-0 60418-3 0 9991
2 60495 97.4007 14.8247 0005022 62.1932 297.9818 15.32662946 65998Epoch: 2025-10-23T15:47Z
TLE epoch observation values (Epoch: 2025-10-23T15:47:20.642Z)
Latitude
-0.00009°
Longitude
105.67473°
Altitude
469.367 km
Speed
7.632 km/s
True Right ascension
00h 59m 17s
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
02:11:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.256 km
Perigee altitude
461.383 km
Semi-major axis
6,842.957 km
Eccentricity
0.0005
Inclination
97.4007°
RAAN
14.8247°
Arg. of periapsis
62.1932°
True anomaly
297.93096°
Mean anomaly
297.9818°
Eccentric anomaly
297.95638°
Mean motion
3.83422 °/min
Orbital period
93.89 mins
BSTAR
0.00060418
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-24 17:26:24.279Z | 54.881° ENE | 2025-10-24 17:28:24.279Z | 96.65° ESE | 18.658° | 2025-10-24 17:30:24.279Z | 137.088° SSE |
| 5 mins | 2025-10-25 05:32:24.279Z | 182.446° SSW | 2025-10-25 05:34:24.279Z | 299.114° NW | 41.385° | 2025-10-25 05:37:24.279Z | 342.58° N |
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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