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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4BE 34
1 60495U 24149AD 25306.44983227 .00015641 00000-0 49181-3 0 9992
2 60495 97.4003 24.6183 0004235 30.2575 329.8911 15.33048903 67494Epoch: 2025-11-02T10:47Z
TLE epoch observation values (Epoch: 2025-11-02T10:47:45.508Z)
Latitude
-0°
Longitude
-179.28671°
Altitude
467.322 km
Speed
7.634 km/s
True Right ascension
01h 38m 28s
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
23:11:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.568 km
Perigee altitude
460.773 km
Semi-major axis
6,841.807 km
Eccentricity
0.00042
Inclination
97.4003°
RAAN
24.6183°
Arg. of periapsis
30.2575°
True anomaly
329.86674°
Mean anomaly
329.8911°
Eccentric anomaly
329.87892°
Mean motion
3.83519 °/min
Orbital period
93.87 mins
BSTAR
0.00049181
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-03 05:43:13.183Z | 189.635° SSW | 2025-11-03 05:46:13.183Z | 276.678° WNW | 34.794° | 2025-11-03 05:49:13.183Z | 334.985° NNW |
| 4 mins | 2025-11-03 18:42:13.183Z | 333.278° NNW | 2025-11-03 18:43:13.183Z | 303.766° NW | 29.32° | 2025-11-03 18:46:13.183Z | 224.237° 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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