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, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4BE 34
1 60495U 24149AD 25260.79692036 .00011857 00000-0 39649-3 0 9997
2 60495 97.4043 338.9976 0005688 160.6809 199.4649 15.31129334 60500Epoch: 2025-09-17T19:07Z
TLE epoch observation values (Epoch: 2025-09-17T19:07:33.919Z)
Latitude
0.00002°
Longitude
55.13855°
Altitude
479.222 km
Speed
7.624 km/s
True Right ascension
22h 35m 59s
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
23:04:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.287 km
Perigee altitude
465.498 km
Semi-major axis
6,847.53 km
Eccentricity
0.00057
Inclination
97.4043°
RAAN
338.9976°
Arg. of periapsis
160.6809°
True anomaly
199.44319°
Mean anomaly
199.4649°
Eccentric anomaly
199.45405°
Mean motion
3.83038 °/min
Orbital period
93.99 mins
BSTAR
0.00039649
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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 | 2025-09-18 17:39:45.797Z | 43.995° NE | 2025-09-18 17:41:45.797Z | 94.731° ESE | 27.183° | 2025-09-18 17:44:45.797Z | 160.074° S |
| 4 mins | 2025-09-19 05:46:45.797Z | 210.529° SW | 2025-09-19 05:47:45.797Z | 240.148° WSW | 31.04° | 2025-09-19 05:50:45.797Z | 326.513° NNW |
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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