FLOCK 4BE 9, 60514
Orbit data source: Space-Track
FLOCK 4BE 9, 60514 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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60514 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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4BE 9
1 60514U 24149AY 26129.49808830 .00012388 00000-0 31602-3 0 9993
2 60514 97.3781 213.4316 0004162 91.5942 268.5781 15.39646976 96363Epoch: 2026-05-09T11:57Z
TLE epoch observation values (Epoch: 2026-05-09T11:57:14.829Z)
Latitude
0.00004°
Longitude
166.80515°
Altitude
450.342 km
Speed
7.642 km/s
True Right ascension
14h 13m 43s
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
04:45:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
446.93 km
Perigee altitude
441.252 km
Semi-major axis
6,822.228 km
Eccentricity
0.00042
Inclination
97.3781°
RAAN
213.4316°
Arg. of periapsis
91.5942°
True anomaly
268.53042°
Mean anomaly
268.5781°
Eccentric anomaly
268.55426°
Mean motion
3.85171 °/min
Orbital period
93.46 mins
BSTAR
0.00031602
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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 9 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 | 2026-05-10 05:14:31.230Z | 143.167° SSE | 2026-05-10 05:17:31.230Z | 69.866° E | 32.693° | 2026-05-10 05:20:31.230Z | 3.818° NNE |
| 4 mins | 2026-05-10 18:10:31.230Z | 42.95° NE | 2026-05-10 18:11:31.230Z | 79.268° E | 35.209° | 2026-05-10 18:14:31.230Z | 171.894° S |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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