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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4BE 34
1 60495U 24149AD 26035.19587506 .00017786 00000-0 49708-3 0 9991
2 60495 97.3881 118.6190 0004284 53.8208 306.3432 15.36742764 81872Epoch: 2026-02-04T04:42Z
TLE epoch observation values (Epoch: 2026-02-04T04:42:03.605Z)
Latitude
0°
Longitude
-86.26195°
Altitude
457.128 km
Speed
7.639 km/s
True Right ascension
07h 54m 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
12:22:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
455.618 km
Perigee altitude
449.765 km
Semi-major axis
6,830.829 km
Eccentricity
0.00043
Inclination
97.3881°
RAAN
118.619°
Arg. of periapsis
53.8208°
True anomaly
306.30365°
Mean anomaly
306.3432°
Eccentric anomaly
306.32342°
Mean motion
3.84444 °/min
Orbital period
93.64 mins
BSTAR
0.00049708
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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 | 2026-02-04 17:46:24.539Z | 41.304° NE | 2026-02-04 17:48:24.539Z | 84.064° E | 24.996° | 2026-02-04 17:51:24.539Z | 155.523° SSE |
| 5 mins | 2026-02-05 05:50:24.539Z | 194.548° SSW | 2026-02-05 05:52:24.539Z | 251.682° W | 34.76° | 2026-02-05 05:55:24.539Z | 332.492° 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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