FLOCK 4Q 9, 58322
Orbit data source: Space-Track
FLOCK 4Q 9, 58322 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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58322 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 4Q 9
1 58322U 23174BU 25289.20323597 .00022963 00000-0 63510-3 0 9994
2 58322 97.4081 8.8372 0006878 301.5226 58.5346 15.37001372107959Epoch: 2025-10-16T04:52Z
TLE epoch observation values (Epoch: 2025-10-16T04:52:39.587Z)
Latitude
-0.00005°
Longitude
-89.29407°
Altitude
455.644 km
Speed
7.641 km/s
True Right ascension
00h 35m 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
05:40:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.623 km
Perigee altitude
447.228 km
Semi-major axis
6,830.063 km
Eccentricity
0.00069
Inclination
97.4081°
RAAN
8.8372°
Arg. of periapsis
301.5226°
True anomaly
58.60186°
Mean anomaly
58.5346°
Eccentric anomaly
58.56823°
Mean motion
3.84509 °/min
Orbital period
93.63 mins
BSTAR
0.0006351
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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 9 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 17:56:04.671Z | 27.014° NE | 2025-10-16 17:59:04.671Z | 91.376° ESE | 33.636° | 2025-10-16 18:02:04.671Z | 169.215° S |
| 4 mins | 2025-10-17 06:01:04.671Z | 213.948° SW | 2025-10-17 06:03:04.671Z | 271.898° WNW | 26.469° | 2025-10-17 06:05:04.671Z | 318.426° NNW |
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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