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: 19 hours ago
TLE from 19 hours ago
0 FLOCK 4BE 27
1 60513U 24149AX 26129.18832657 .00007412 00000-0 22923-3 0 9990
2 60513 97.3818 211.0424 0005459 88.6105 271.5763 15.33778151 96162Epoch: 2026-05-09T04:31Z
TLE epoch observation values (Epoch: 2026-05-09T04:31:11.415Z)
Latitude
-0.00004°
Longitude
-83.7645°
Altitude
467.561 km
Speed
7.633 km/s
True Right ascension
14h 04m 10s
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
07:51:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.232 km
Perigee altitude
457.765 km
Semi-major axis
6,839.636 km
Eccentricity
0.00055
Inclination
97.3818°
RAAN
211.0424°
Arg. of periapsis
88.6105°
True anomaly
271.51377°
Mean anomaly
271.5763°
Eccentric anomaly
271.54503°
Mean motion
3.83702 °/min
Orbital period
93.82 mins
BSTAR
0.00022923
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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 | 2026-05-10 05:41:25.491Z | 179.9° S | 2026-05-10 05:44:25.491Z | 237.181° WSW | 39.446° | 2026-05-10 05:47:25.491Z | 337.239° NNW |
| 4 mins | 2026-05-10 18:40:25.491Z | 343.804° N | 2026-05-10 18:42:25.491Z | 264.148° W | 33.772° | 2026-05-10 18:44:25.491Z | 218.451° SW |
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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