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
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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4BE 27
1 60513U 24149AX 26084.48681633 .00009155 00000-0 29031-3 0 9992
2 60513 97.3844 166.3865 0003093 222.5602 137.5401 15.32921333 89315Epoch: 2026-03-25T11:41Z
TLE epoch observation values (Epoch: 2026-03-25T11:41:00.930Z)
Latitude
-0.00003°
Longitude
168.18321°
Altitude
471.773 km
Speed
7.629 km/s
True Right ascension
11h 05m 32s
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
23:38:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.166 km
Perigee altitude
461.933 km
Semi-major axis
6,842.186 km
Eccentricity
0.00031
Inclination
97.3844°
RAAN
166.3865°
Arg. of periapsis
222.5602°
True anomaly
137.56402°
Mean anomaly
137.5401°
Eccentric anomaly
137.55206°
Mean motion
3.83487 °/min
Orbital period
93.88 mins
BSTAR
0.00029031
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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 | 2026-03-25 18:30:54.735Z | 358.265° N | 2026-03-25 18:32:54.735Z | 313.857° NW | 37.972° | 2026-03-25 18:35:54.735Z | 209.791° SW |
| 5 mins | 2026-03-26 05:03:54.735Z | 132.309° SE | 2026-03-26 05:05:54.735Z | 67.923° E | 32.802° | 2026-03-26 05:08:54.735Z | 4.204° NNE |
| 6 mins | 2026-03-26 18:00:54.735Z | 25.296° NE | 2026-03-26 18:03:54.735Z | 122.891° SE | 37.489° | 2026-03-26 18:06:54.735Z | 177.734° 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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