FLOCK 4BE 13, 60512
Orbit data source: Space-Track
FLOCK 4BE 13, 60512 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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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: 14 hours ago
TLE from 14 hours ago
0 FLOCK 4BE 13
1 60512U 24149AW 26260.23840144 .00030403 00000-0 65082-3 0 9990
2 60512 97.3671 345.7411 0003089 300.1670 59.9272 15.44736409116567Epoch: 2026-09-17T05:43Z
TLE epoch observation values (Epoch: 2026-09-17T05:43:17.884Z)
Latitude
-0.00005°
Longitude
-96.26192°
Altitude
434.224 km
Speed
7.652 km/s
True Right ascension
23h 02m 57s
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
12:11:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
431.187 km
Perigee altitude
426.981 km
Semi-major axis
6,807.221 km
Eccentricity
0.00031
Inclination
97.3671°
RAAN
345.7411°
Arg. of periapsis
300.167°
True anomaly
59.95784°
Mean anomaly
59.9272°
Eccentric anomaly
59.94252°
Mean motion
3.86446 °/min
Orbital period
93.16 mins
BSTAR
0.00065082
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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 13 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 | 2026-09-18 05:11:37.438Z | 113.647° SE | 2026-09-18 05:13:37.438Z | 65.02° ENE | 22.578° | 2026-09-18 05:15:37.438Z | 22.537° NE |
| 4 mins | 2026-09-18 18:03:37.438Z | 56.129° ENE | 2026-09-18 18:05:37.438Z | 109.105° ESE | 23.124° | 2026-09-18 18:07:37.438Z | 149.093° 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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