FLOCK 4BE 3, 60561
Orbit data source: Space-Track
FLOCK 4BE 3, 60561 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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60561 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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4BE 3
1 60561U 24149CX 26129.76884565 .00012626 00000-0 31406-3 0 9991
2 60561 97.3692 213.3494 0005300 79.7274 280.4569 15.40407817 96428Epoch: 2026-05-09T18:27Z
TLE epoch observation values (Epoch: 2026-05-09T18:27:08.264Z)
Latitude
-0.00007°
Longitude
68.98344°
Altitude
447.369 km
Speed
7.644 km/s
True Right ascension
14h 13m 23s
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
10:39:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
445.456 km
Perigee altitude
438.227 km
Semi-major axis
6,819.979 km
Eccentricity
0.00053
Inclination
97.3692°
RAAN
213.3494°
Arg. of periapsis
79.7274°
True anomaly
280.39717°
Mean anomaly
280.4569°
Eccentric anomaly
280.42703°
Mean motion
3.85362 °/min
Orbital period
93.42 mins
BSTAR
0.00031406
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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 3 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 | 2026-05-10 05:29:38.354Z | 159.955° S | 2026-05-10 05:32:38.354Z | 44.009° NE | 43.022° | 2026-05-10 05:35:38.354Z | 352.567° N |
| 5 mins | 2026-05-10 18:24:38.354Z | 14.593° NNE | 2026-05-10 18:26:38.354Z | 154.555° SSE | 44.646° | 2026-05-10 18:29:38.354Z | 190.893° 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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