FLOCK 4BE 15, 60491
Orbit data source: Space-Track
FLOCK 4BE 15, 60491 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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60491 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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4BE 15
1 60491U 24149Z 26130.78221905 .00076700 00000-0 12713-2 0 9992
2 60491 97.3692 214.9911 0003914 147.1687 212.9810 15.51881094 96613Epoch: 2026-05-10T18:46Z
TLE epoch observation values (Epoch: 2026-05-10T18:46:23.725Z)
Latitude
0.00002°
Longitude
64.81188°
Altitude
416.599 km
Speed
7.66 km/s
True Right ascension
14h 19m 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
08:44:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
410.812 km
Perigee altitude
405.5 km
Semi-major axis
6,786.293 km
Eccentricity
0.00039
Inclination
97.3692°
RAAN
214.9911°
Arg. of periapsis
147.1687°
True anomaly
212.95659°
Mean anomaly
212.981°
Eccentric anomaly
212.9688°
Mean motion
3.88235 °/min
Orbital period
92.73 mins
BSTAR
0.0012713
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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 15 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 | 2026-05-11 05:43:55.347Z | 173.293° S | 2026-05-11 05:46:55.347Z | 304.453° NW | 42.742° | 2026-05-11 05:48:55.347Z | 342.456° N |
| 4 mins | 2026-05-11 18:33:55.347Z | 3.144° NNE | 2026-05-11 18:34:55.347Z | 315.935° NNW | 44.059° | 2026-05-11 18:37:55.347Z | 197.225° SSW |
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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