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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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: 19 hours ago
TLE from 19 hours ago
0 FLOCK 4Q 9
1 58322U 23174BU 26234.19821204 .00027753 00000-0 44349-3 0 9992
2 58322 97.3825 324.4915 0004836 240.3897 119.6874 15.53132235155825Epoch: 2026-08-22T04:45Z
TLE epoch observation values (Epoch: 2026-08-22T04:45:25.520Z)
Latitude
-0.00007°
Longitude
-77.37689°
Altitude
412.35 km
Speed
7.663 km/s
True Right ascension
21h 37m 57s
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
14:27:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
407.788 km
Perigee altitude
401.228 km
Semi-major axis
6,782.645 km
Eccentricity
0.00048
Inclination
97.3825°
RAAN
324.4915°
Arg. of periapsis
240.3897°
True anomaly
119.73553°
Mean anomaly
119.6874°
Eccentric anomaly
119.71147°
Mean motion
3.88548 °/min
Orbital period
92.65 mins
BSTAR
0.00044349
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-23 05:37:55.923Z | 133.268° SE | 2026-08-23 05:40:55.923Z | 59.681° ENE | 25.041° | 2026-08-23 05:42:55.923Z | 15.132° NNE |
| 4 mins | 2026-08-23 18:26:55.923Z | 57.097° ENE | 2026-08-23 18:27:55.923Z | 84.982° E | 23.328° | 2026-08-23 18:30:55.923Z | 156.455° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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