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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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 2
1 58320U 23174BS 25343.57687713 .00030665 00000-0 75748-3 0 9990
2 58320 97.3998 63.6858 0008417 106.9948 253.2221 15.40409252116320Epoch: 2025-12-09T13:50Z
TLE epoch observation values (Epoch: 2025-12-09T13:50:42.184Z)
Latitude
-0.00001°
Longitude
137.45047°
Altitude
449.681 km
Speed
7.642 km/s
True Right ascension
04h 14m 44s
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
18:32:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.579 km
Perigee altitude
436.099 km
Semi-major axis
6,819.976 km
Eccentricity
0.00084
Inclination
97.3998°
RAAN
63.6858°
Arg. of periapsis
106.9948°
True anomaly
253.12978°
Mean anomaly
253.2221°
Eccentric anomaly
253.17594°
Mean motion
3.85362 °/min
Orbital period
93.42 mins
BSTAR
0.00075748
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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 | 2025-12-10 05:33:46.552Z | 167.599° S | 2025-12-10 05:36:46.552Z | 342.659° N | 44.244° | 2025-12-10 05:39:46.552Z | 347.837° N |
| 5 mins | 2025-12-10 18:28:46.552Z | 5.914° NNE | 2025-12-10 18:30:46.552Z | 244.954° WSW | 43.766° | 2025-12-10 18:33:46.552Z | 197.611° 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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