FLOCK 4BE 22, 60494
Orbit data source: Space-Track
FLOCK 4BE 22, 60494 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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60494 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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4BE 22
1 60494U 24149AC 26140.53471454 .00012237 00000-0 30610-3 0 9997
2 60494 97.3730 223.8535 0003470 36.5597 323.5886 15.40252054 98045Epoch: 2026-05-20T12:49Z
TLE epoch observation values (Epoch: 2026-05-20T12:49:59.336Z)
Latitude
0.00004°
Longitude
153.16338°
Altitude
446.578 km
Speed
7.645 km/s
True Right ascension
14h 55m 24s
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
07:12:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
444.669 km
Perigee altitude
439.936 km
Semi-major axis
6,820.439 km
Eccentricity
0.00035
Inclination
97.373°
RAAN
223.8535°
Arg. of periapsis
36.5597°
True anomaly
323.56499°
Mean anomaly
323.5886°
Eccentric anomaly
323.5768°
Mean motion
3.85323 °/min
Orbital period
93.43 mins
BSTAR
0.0003061
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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 22 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 | 2026-05-21 06:08:05.682Z | 225.457° WSW | 2026-05-21 06:09:05.682Z | 257.481° W | 26.707° | 2026-05-21 06:12:05.682Z | 325.392° NNW |
| 4 mins | 2026-05-21 19:02:05.682Z | 322.35° NNW | 2026-05-21 19:03:05.682Z | 293.31° NW | 24.424° | 2026-05-21 19:06:05.682Z | 228.888° WSW |
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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