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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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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4BE 3
1 60561U 24149CX 26035.14733203 .00019799 00000-0 55048-3 0 9997
2 60561 97.3801 118.1871 0005107 56.5606 303.6125 15.36876621 81875Epoch: 2026-02-04T03:32Z
TLE epoch observation values (Epoch: 2026-02-04T03:32:09.487Z)
Latitude
-0.00012°
Longitude
-69.1705°
Altitude
456.535 km
Speed
7.64 km/s
True Right ascension
07h 52m 44s
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
12:22:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
455.783 km
Perigee altitude
448.806 km
Semi-major axis
6,830.431 km
Eccentricity
0.00051
Inclination
97.3801°
RAAN
118.1871°
Arg. of periapsis
56.5606°
True anomaly
303.56375°
Mean anomaly
303.6125°
Eccentric anomaly
303.58812°
Mean motion
3.84478 °/min
Orbital period
93.63 mins
BSTAR
0.00055048
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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 | 2026-02-04 18:09:38.576Z | 19.147° NNE | 2026-02-04 18:12:38.576Z | 134.4° SE | 41.755° | 2026-02-04 18:15:38.576Z | 184.485° SSW |
| 4 mins | 2026-02-05 06:14:38.576Z | 230.597° WSW | 2026-02-05 06:15:38.576Z | 252.393° W | 18.649° | 2026-02-05 06:18:38.576Z | 314.063° NW |
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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