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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4BE 9
1 60514U 24149AY 26084.50308051 .00017727 00000-0 47359-3 0 9993
2 60514 97.3805 168.1231 0002554 206.8189 153.2925 15.38148817 89440Epoch: 2026-03-25T12:04Z
TLE epoch observation values (Epoch: 2026-03-25T12:04:26.156Z)
Latitude
0.00007°
Longitude
164.04866°
Altitude
456.258 km
Speed
7.638 km/s
True Right ascension
11h 12m 29s
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
23:17:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.268 km
Perigee altitude
446.781 km
Semi-major axis
6,826.661 km
Eccentricity
0.00026
Inclination
97.3805°
RAAN
168.1231°
Arg. of periapsis
206.8189°
True anomaly
153.30565°
Mean anomaly
153.2925°
Eccentric anomaly
153.29908°
Mean motion
3.84796 °/min
Orbital period
93.56 mins
BSTAR
0.00047359
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-25 18:52:11.000Z | 351.287° N | 2026-03-25 18:55:11.000Z | 284.132° WNW | 28.457° | 2026-03-25 18:57:11.000Z | 231.344° WSW |
| 5 mins | 2026-03-26 05:23:11.000Z | 152.756° SSE | 2026-03-26 05:25:11.000Z | 106.397° ESE | 40.208° | 2026-03-26 05:28:11.000Z | 357.274° N |
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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