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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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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: 20 hours ago
TLE from 20 hours ago
0 FLOCK 4BE 27
1 60513U 24149AX 26260.23021241 .00008310 00000-0 24030-3 0 9990
2 60513 97.3765 342.1913 0003292 357.6316 2.4912 15.35877479116264Epoch: 2026-09-17T05:31Z
TLE epoch observation values (Epoch: 2026-09-17T05:31:30.352Z)
Latitude
0.00003°
Longitude
-96.85561°
Altitude
459.179 km
Speed
7.638 km/s
True Right ascension
22h 48m 45s
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
18:13:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.508 km
Perigee altitude
453.009 km
Semi-major axis
6,833.396 km
Eccentricity
0.00033
Inclination
97.3765°
RAAN
342.1913°
Arg. of periapsis
357.6316°
True anomaly
2.49284°
Mean anomaly
2.4912°
Eccentric anomaly
2.49202°
Mean motion
3.84227 °/min
Orbital period
93.69 mins
BSTAR
0.0002403
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-18 05:06:37.549Z | 136.467° SSE | 2026-09-18 05:09:37.549Z | 71.903° E | 32.321° | 2026-09-18 05:12:37.549Z | 8.724° NNE |
| 5 mins | 2026-09-18 18:03:37.549Z | 34.993° NE | 2026-09-18 18:05:37.549Z | 84.728° E | 38.93° | 2026-09-18 18:08:37.549Z | 166.263° S |
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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