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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Edit Public Description
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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4BE 36
1 60486U 24149U 25300.16587524 .00018333 00000-0 57525-3 0 9997
2 60486 97.3961 18.1408 0004544 34.0979 326.0554 15.33079717 66530Epoch: 2025-10-27T03:58Z
TLE epoch observation values (Epoch: 2025-10-27T03:58:51.620Z)
Latitude
-0.00008°
Longitude
-77.3459°
Altitude
467.158 km
Speed
7.634 km/s
True Right ascension
01h 12m 33s
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
16:36:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.687 km
Perigee altitude
460.469 km
Semi-major axis
6,841.715 km
Eccentricity
0.00045
Inclination
97.3961°
RAAN
18.1408°
Arg. of periapsis
34.0979°
True anomaly
326.02631°
Mean anomaly
326.0554°
Eccentric anomaly
326.04086°
Mean motion
3.83527 °/min
Orbital period
93.87 mins
BSTAR
0.00057525
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-28 05:10:51.123Z | 152.121° SSE | 2025-10-28 05:12:51.123Z | 112.964° SE | 38.855° | 2025-10-28 05:15:51.123Z | 358.658° N |
| 5 mins | 2025-10-28 18:08:51.123Z | 16.487° NNE | 2025-10-28 18:10:51.123Z | 60.99° ENE | 44.135° | 2025-10-28 18:13:51.123Z | 188.447° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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