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
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: 1 day ago
TLE from 1 day ago
0 FLOCK 4BE 36
1 60486U 24149U 26083.65625150 .00019202 00000-0 48562-3 0 9995
2 60486 97.3758 167.2440 0003990 191.5170 168.5986 15.39813485 89337Epoch: 2026-03-24T15:45Z
TLE epoch observation values (Epoch: 2026-03-24T15:45:00.129Z)
Latitude
0.00004°
Longitude
108.86268°
Altitude
452.448 km
Speed
7.639 km/s
True Right ascension
11h 08m 58s
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
21:56:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
446.32 km
Perigee altitude
440.877 km
Semi-major axis
6,821.736 km
Eccentricity
0.0004
Inclination
97.3758°
RAAN
167.244°
Arg. of periapsis
191.517°
True anomaly
168.60763°
Mean anomaly
168.5986°
Eccentric anomaly
168.60312°
Mean motion
3.85213 °/min
Orbital period
93.45 mins
BSTAR
0.00048562
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-25 18:50:37.723Z | 329.162° NNW | 2026-03-25 18:51:37.723Z | 293.54° NW | 30.302° | 2026-03-25 18:54:37.723Z | 220.435° SW |
| 5 mins | 2026-03-26 05:19:37.723Z | 143.853° SSE | 2026-03-26 05:21:37.723Z | 63.245° ENE | 38.407° | 2026-03-26 05:24:37.723Z | 358.382° N |
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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