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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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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4BE 22
1 60494U 24149AC 26035.16626456 .00020608 00000-0 58305-3 0 9995
2 60494 97.3834 117.8773 0004609 44.3664 315.7949 15.36326532 81844Epoch: 2026-02-04T03:59Z
TLE epoch observation values (Epoch: 2026-02-04T03:59:25.257Z)
Latitude
-0.00002°
Longitude
-76.31468°
Altitude
457.838 km
Speed
7.639 km/s
True Right ascension
07h 51m 30s
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
12:22:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.075 km
Perigee altitude
450.777 km
Semi-major axis
6,832.063 km
Eccentricity
0.00046
Inclination
97.3834°
RAAN
117.8773°
Arg. of periapsis
44.3664°
True anomaly
315.75806°
Mean anomaly
315.7949°
Eccentric anomaly
315.77648°
Mean motion
3.8434 °/min
Orbital period
93.67 mins
BSTAR
0.00058305
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-04 18:36:36.572Z | 357.46° N | 2026-02-04 18:39:36.572Z | 286.492° WNW | 35.021° | 2026-02-04 18:42:36.572Z | 213.935° SW |
| 5 mins | 2026-02-05 05:08:36.572Z | 140.905° SSE | 2026-02-05 05:10:36.572Z | 82.884° E | 35.482° | 2026-02-05 05:13:36.572Z | 2.709° NNE |
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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