FLOCK 4BE 27, 60513
Orbit data source: Space-Track
FLOCK 4BE 27, 60513 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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60513 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: 10 hours ago
TLE from 10 hours ago
0 FLOCK 4BE 27
1 60513U 24149AX 25300.47562954 .00010551 00000-0 37638-3 0 9999
2 60513 97.4037 17.8167 0005408 63.6530 296.5264 15.29057356 66512Epoch: 2025-10-27T11:24Z
TLE epoch observation values (Epoch: 2025-10-27T11:24:54.392Z)
Latitude
-0.0001°
Longitude
170.51314°
Altitude
480.077 km
Speed
7.626 km/s
True Right ascension
01h 11m 16s
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
16:36:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.289 km
Perigee altitude
471.876 km
Semi-major axis
6,853.72 km
Eccentricity
0.00054
Inclination
97.4037°
RAAN
17.8167°
Arg. of periapsis
63.653°
True anomaly
296.47094°
Mean anomaly
296.5264°
Eccentric anomaly
296.49867°
Mean motion
3.8252 °/min
Orbital period
94.11 mins
BSTAR
0.00037638
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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 27 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 | 2025-10-28 04:49:52.668Z | 132.544° SE | 2025-10-28 04:52:52.668Z | 54.692° ENE | 27.741° | 2025-10-28 04:54:52.668Z | 13.355° NNE |
| 5 mins | 2025-10-28 17:49:52.668Z | 33.275° NE | 2025-10-28 17:51:52.668Z | 88.117° E | 35.044° | 2025-10-28 17:54:52.668Z | 170.224° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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