FLOCK 4Q 2, 58320
Orbit data source: Space-Track
FLOCK 4Q 2, 58320 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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58320 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: 1 day ago
TLE from 1 day ago
0 FLOCK 4Q 2
1 58320U 23174BS 26079.81398049 .00027157 00000-0 56484-3 0 9993
2 58320 97.3857 166.4153 0007767 105.5265 254.6842 15.45580513131931Epoch: 2026-03-20T19:32Z
TLE epoch observation values (Epoch: 2026-03-20T19:32:07.914Z)
Latitude
-0.00002°
Longitude
55.03868°
Altitude
434.199 km
Speed
7.65 km/s
True Right ascension
11h 05m 39s
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
09:38:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
431.889 km
Perigee altitude
421.319 km
Semi-major axis
6,804.741 km
Eccentricity
0.00078
Inclination
97.3857°
RAAN
166.4153°
Arg. of periapsis
105.5265°
True anomaly
254.59838°
Mean anomaly
254.6842°
Eccentric anomaly
254.64129°
Mean motion
3.86657 °/min
Orbital period
93.11 mins
BSTAR
0.00056484
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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 2 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 | 2026-03-22 05:50:31.389Z | 172.976° S | 2026-03-22 05:53:31.389Z | 266.347° W | 43.869° | 2026-03-22 05:56:31.389Z | 344.1° N |
| 4 mins | 2026-03-22 18:43:31.389Z | 359.853° N | 2026-03-22 18:44:31.389Z | 334.885° NNW | 40.547° | 2026-03-22 18:47:31.389Z | 201.463° SSW |
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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