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: 10 hours ago
TLE from 10 hours ago
0 FLOCK 4Q 9
1 58322U 23174BU 26176.48459122 .00038548 00000-0 67859-3 0 9990
2 58322 97.3864 265.2118 0007603 113.6213 246.5837 15.50327345146873Epoch: 2026-06-25T11:37Z
TLE epoch observation values (Epoch: 2026-06-25T11:37:48.681Z)
Latitude
-0.00007°
Longitude
177.13219°
Altitude
420.958 km
Speed
7.657 km/s
True Right ascension
17h 40m 50s
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
08:38:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
417.857 km
Perigee altitude
407.531 km
Semi-major axis
6,790.831 km
Eccentricity
0.00076
Inclination
97.3864°
RAAN
265.2118°
Arg. of periapsis
113.6213°
True anomaly
246.50378°
Mean anomaly
246.5837°
Eccentric anomaly
246.54374°
Mean motion
3.87846 °/min
Orbital period
92.82 mins
BSTAR
0.00067859
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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 | 2026-06-26 06:20:57.942Z | 194.213° SSW | 2026-06-26 06:22:57.942Z | 242.633° WSW | 31.761° | 2026-06-26 06:25:57.942Z | 330.369° NNW |
| 4 mins | 2026-06-26 19:10:57.942Z | 340.995° N | 2026-06-26 19:11:57.942Z | 309.161° NW | 31.781° | 2026-06-26 19:14:57.942Z | 216.814° SW |
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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