FLOCK 4BE 36, 60486
Orbit data source: Space-Track
FLOCK 4BE 36, 60486 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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60486 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 36
1 60486U 24149U 26220.17336237 .00019407 00000-0 41511-3 0 9994
2 60486 97.3724 305.2823 0004106 88.4154 271.7565 15.44845148110371Epoch: 2026-08-08T04:09Z
TLE epoch observation values (Epoch: 2026-08-08T04:09:38.508Z)
Latitude
-0.00004°
Longitude
-73.81665°
Altitude
434.873 km
Speed
7.651 km/s
True Right ascension
20h 21m 07s
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
00:45:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
431.559 km
Perigee altitude
425.97 km
Semi-major axis
6,806.901 km
Eccentricity
0.00041
Inclination
97.3724°
RAAN
305.2823°
Arg. of periapsis
88.4154°
True anomaly
271.70947°
Mean anomaly
271.7565°
Eccentric anomaly
271.73299°
Mean motion
3.86473 °/min
Orbital period
93.15 mins
BSTAR
0.00041511
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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 36 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-08 18:42:14.597Z | 7.681° NNE | 2026-08-08 18:45:14.597Z | 269.705° W | 43.816° | 2026-08-08 18:48:14.597Z | 198.592° SSW |
| 4 mins | 2026-08-09 05:11:14.597Z | 114.615° SE | 2026-08-09 05:13:14.597Z | 60.994° ENE | 22.314° | 2026-08-09 05:15:14.597Z | 19.017° NNE |
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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