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: 18 hours ago
TLE from 18 hours ago
0 FLOCK 4BE 23
1 60490U 24149Y 26083.96861805 .00013588 00000-0 39746-3 0 9998
2 60490 97.3793 166.1070 0003604 190.0805 170.0367 15.35376350 89263Epoch: 2026-03-24T23:14Z
TLE epoch observation values (Epoch: 2026-03-24T23:14:48.599Z)
Latitude
-0.00001°
Longitude
-5.03415°
Altitude
465.343 km
Speed
7.632 km/s
True Right ascension
11h 04m 25s
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
22:03:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.21 km
Perigee altitude
454.284 km
Semi-major axis
6,834.884 km
Eccentricity
0.00036
Inclination
97.3793°
RAAN
166.107°
Arg. of periapsis
190.0805°
True anomaly
170.04384°
Mean anomaly
170.0367°
Eccentric anomaly
170.04027°
Mean motion
3.84102 °/min
Orbital period
93.73 mins
BSTAR
0.00039746
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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 | 2026-03-25 18:34:36.707Z | 356.918° N | 2026-03-25 18:37:36.707Z | 257.555° W | 35.567° | 2026-03-25 18:39:36.707Z | 214.235° SW |
| 5 mins | 2026-03-26 05:06:36.707Z | 136.848° SSE | 2026-03-26 05:08:36.707Z | 77.297° E | 33.965° | 2026-03-26 05:11:36.707Z | 4.05° 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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