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: 1 day ago
TLE from 1 day ago
0 FLOCK 4BE 27
1 60513U 24149AX 26173.67215797 .00007027 00000-0 21249-3 0 9995
2 60513 97.3821 255.5261 0002311 284.1341 75.9646 15.34526522102985Epoch: 2026-06-22T16:07Z
TLE epoch observation values (Epoch: 2026-06-22T16:07:54.448Z)
Latitude
0.00005°
Longitude
102.69451°
Altitude
465.055 km
Speed
7.634 km/s
True Right ascension
17h 02m 06s
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
12:20:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.853 km
Perigee altitude
457.693 km
Semi-major axis
6,837.41 km
Eccentricity
0.00023
Inclination
97.3821°
RAAN
255.5261°
Arg. of periapsis
284.1341°
True anomaly
75.99029°
Mean anomaly
75.9646°
Eccentric anomaly
75.97745°
Mean motion
3.83889 °/min
Orbital period
93.78 mins
BSTAR
0.00021249
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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 | 2026-06-24 05:49:21.462Z | 188.888° SSW | 2026-06-24 05:51:21.462Z | 231.46° WSW | 35.239° | 2026-06-24 05:54:21.462Z | 332.21° NNW |
| 5 mins | 2026-06-24 18:46:21.462Z | 350.208° N | 2026-06-24 18:48:21.462Z | 307.05° NW | 30.781° | 2026-06-24 18:51:21.462Z | 221.684° 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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