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: 22 hours ago
TLE from 22 hours ago
0 FLOCK 4BE 27
1 60513U 24149AX 26034.20491772 .00011106 00000-0 36444-3 0 9995
2 60513 97.3928 116.1997 0005186 70.2327 289.9473 15.31757431 81615Epoch: 2026-02-03T04:55Z
TLE epoch observation values (Epoch: 2026-02-03T04:55:04.891Z)
Latitude
-0.00003°
Longitude
-90.95987°
Altitude
472.465 km
Speed
7.63 km/s
True Right ascension
07h 44m 47s
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
04:27:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.069 km
Perigee altitude
463.968 km
Semi-major axis
6,845.655 km
Eccentricity
0.00052
Inclination
97.3928°
RAAN
116.1997°
Arg. of periapsis
70.2327°
True anomaly
289.89143°
Mean anomaly
289.9473°
Eccentric anomaly
289.91936°
Mean motion
3.83196 °/min
Orbital period
93.95 mins
BSTAR
0.00036444
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-04 04:35:38.806Z | 104.735° ESE | 2026-02-04 04:37:38.806Z | 61.798° ENE | 17.883° | 2026-02-04 04:39:38.806Z | 25.146° NE |
| 4 mins | 2026-02-04 06:08:38.806Z | 225.606° WSW | 2026-02-04 06:10:38.806Z | 272.34° WNW | 20.254° | 2026-02-04 06:12:38.806Z | 311.919° NW |
| 4 mins | 2026-02-04 17:33:38.806Z | 54.104° ENE | 2026-02-04 17:35:38.806Z | 101.627° ESE | 21.604° | 2026-02-04 17:37:38.806Z | 143.719° SSE |
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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