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: 16 hours ago
TLE from 16 hours ago
0 FLOCK 4BE 9
1 60514U 24149AY 26265.02514469 .00026777 00000-0 58596-3 0 9993
2 60514 97.3743 350.4089 0001523 315.4850 44.6275 15.44112371117249Epoch: 2026-09-22T00:36Z
TLE epoch observation values (Epoch: 2026-09-22T00:36:12.501Z)
Latitude
-0.00008°
Longitude
-19.53973°
Altitude
436.373 km
Speed
7.65 km/s
True Right ascension
23h 21m 38s
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
09:22:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
431.957 km
Perigee altitude
429.883 km
Semi-major axis
6,809.057 km
Eccentricity
0.00015
Inclination
97.3743°
RAAN
350.4089°
Arg. of periapsis
315.485°
True anomaly
44.63976°
Mean anomaly
44.6275°
Eccentric anomaly
44.63363°
Mean motion
3.86289 °/min
Orbital period
93.19 mins
BSTAR
0.00058596
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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 | 2026-09-22 18:16:53.773Z | 36.126° NE | 2026-09-22 18:18:53.773Z | 87.854° E | 36.837° | 2026-09-22 18:21:53.773Z | 166.101° S |
| 4 mins | 2026-09-23 06:17:53.773Z | 211.252° SW | 2026-09-23 06:18:53.773Z | 240.162° WSW | 33.605° | 2026-09-23 06:21:53.773Z | 325.838° NNW |
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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