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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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 23
1 60490U 24149Y 25300.46597331 .00015169 00000-0 52024-3 0 9995
2 60490 97.4002 17.6983 0004232 38.6321 321.5221 15.30256270 66516Epoch: 2025-10-27T11:11Z
TLE epoch observation values (Epoch: 2025-10-27T11:11:00.093Z)
Latitude
-0.00014°
Longitude
173.88051°
Altitude
475.881 km
Speed
7.629 km/s
True Right ascension
01h 10m 47s
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
13:22:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.898 km
Perigee altitude
469.1 km
Semi-major axis
6,850.136 km
Eccentricity
0.00042
Inclination
97.4002°
RAAN
17.6983°
Arg. of periapsis
38.6321°
True anomaly
321.49191°
Mean anomaly
321.5221°
Eccentric anomaly
321.50701°
Mean motion
3.8282 °/min
Orbital period
94.04 mins
BSTAR
0.00052024
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-27 18:01:06.444Z | 17.557° NNE | 2025-10-27 18:04:06.444Z | 85.666° E | 43.054° | 2025-10-27 18:07:06.444Z | 184.334° SSW |
| 4 mins | 2025-10-28 17:35:06.444Z | 51.46° ENE | 2025-10-28 17:37:06.444Z | 105.461° ESE | 25.155° | 2025-10-28 17:39:06.444Z | 149.949° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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