FLOCK 4BE 23, 60490
Orbit data source: Space-Track
FLOCK 4BE 23, 60490 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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60490 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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4BE 23
1 60490U 24149Y 26175.19940418 .00011590 00000-0 31394-3 0 9995
2 60490 97.3781 257.6392 0002597 220.6979 139.4072 15.37821056103275Epoch: 2026-06-24T04:47Z
TLE epoch observation values (Epoch: 2026-06-24T04:47:08.521Z)
Latitude
-0.00001°
Longitude
-86.50635°
Altitude
457.017 km
Speed
7.638 km/s
True Right ascension
17h 10m 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
23:17:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
451.268 km
Perigee altitude
447.722 km
Semi-major axis
6,827.632 km
Eccentricity
0.00026
Inclination
97.3781°
RAAN
257.6392°
Arg. of periapsis
220.6979°
True anomaly
139.42656°
Mean anomaly
139.4072°
Eccentric anomaly
139.41688°
Mean motion
3.84714 °/min
Orbital period
93.58 mins
BSTAR
0.00031394
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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 23 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 | 2026-06-24 17:50:55.737Z | 40.438° NE | 2026-06-24 17:52:55.737Z | 82.426° E | 25.024° | 2026-06-24 17:55:55.737Z | 155.528° SSE |
| 4 mins | 2026-06-25 05:54:55.737Z | 200.351° SSW | 2026-06-25 05:56:55.737Z | 279.079° WNW | 34.281° | 2026-06-25 05:58:55.737Z | 328.56° NNW |
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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