FLOCK 4Q 22, 58306
Orbit data source: Space-Track
FLOCK 4Q 22, 58306 is a payload satellite owned by Planet (US) in SSO that was launched on Sat, 11 Nov 2023 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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58306 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 4Q 22
1 58306U 23174BC 25289.14827793 .00027465 00000-0 65189-3 0 9992
2 58306 97.4025 10.0863 0006065 295.6843 64.3778 15.41658919108051Epoch: 2025-10-16T03:33Z
TLE epoch observation values (Epoch: 2025-10-16T03:33:31.213Z)
Latitude
0.00008°
Longitude
-68.20592°
Altitude
442.546 km
Speed
7.647 km/s
True Right ascension
00h 40m 20s
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
05:39:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
442.284 km
Perigee altitude
434.016 km
Semi-major axis
6,816.287 km
Eccentricity
0.00061
Inclination
97.4025°
RAAN
10.0863°
Arg. of periapsis
295.6843°
True anomaly
64.44049°
Mean anomaly
64.3778°
Eccentric anomaly
64.40914°
Mean motion
3.85675 °/min
Orbital period
93.34 mins
BSTAR
0.00065189
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Other satellites on launch #174 in the year 2023 (2023-11-11 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 4Q 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 | 2025-10-16 18:08:01.801Z | 22.776° NE | 2025-10-16 18:11:01.801Z | 93.476° ESE | 38.234° | 2025-10-16 18:14:01.801Z | 176.53° S |
| 4 mins | 2025-10-17 06:11:01.801Z | 222.235° SW | 2025-10-17 06:13:01.801Z | 278.252° WNW | 22.738° | 2025-10-17 06:15:01.801Z | 318.207° 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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