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: 14 hours ago
TLE from 14 hours ago
0 FLOCK 4Q 9
1 58322U 23174BU 25334.80334554 .00022435 00000-0 57152-3 0 9995
2 58322 97.4048 54.8609 0008859 135.9114 224.2839 15.39527858114964Epoch: 2025-11-30T19:16Z
TLE epoch observation values (Epoch: 2025-11-30T19:16:49.054Z)
Latitude
-0.00008°
Longitude
55.74456°
Altitude
454.954 km
Speed
7.637 km/s
True Right ascension
03h 39m 26s
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
06:30:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.488 km
Perigee altitude
438.4 km
Semi-major axis
6,822.581 km
Eccentricity
0.00089
Inclination
97.4048°
RAAN
54.8609°
Arg. of periapsis
135.9114°
True anomaly
224.21308°
Mean anomaly
224.2839°
Eccentric anomaly
224.24848°
Mean motion
3.85141 °/min
Orbital period
93.47 mins
BSTAR
0.00057152
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-01 17:41:30.471Z | 47.829° ENE | 2025-12-01 17:43:30.471Z | 89.503° E | 20.304° | 2025-12-01 17:45:30.471Z | 137.299° SSE |
| 5 mins | 2025-12-02 05:44:30.471Z | 185.787° SSW | 2025-12-02 05:46:30.471Z | 286.624° WNW | 40.411° | 2025-12-02 05:49:30.471Z | 340.838° N |
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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