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: 22 hours ago
TLE from 22 hours ago
0 FLOCK 4Q 2
1 58320U 23174BS 26172.52376442 .00018886 00000-0 34086-3 0 9991
2 58320 97.3827 261.0661 0006868 122.2371 237.9547 15.49766064146279Epoch: 2026-06-21T12:34Z
TLE epoch observation values (Epoch: 2026-06-21T12:34:13.245Z)
Latitude
-0.00003°
Longitude
162.78811°
Altitude
423.02 km
Speed
7.656 km/s
True Right ascension
17h 24m 15s
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
21:36:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
419 km
Perigee altitude
409.67 km
Semi-major axis
6,792.472 km
Eccentricity
0.00069
Inclination
97.3827°
RAAN
261.0661°
Arg. of periapsis
122.2371°
True anomaly
237.88802°
Mean anomaly
237.9547°
Eccentric anomaly
237.92136°
Mean motion
3.87705 °/min
Orbital period
92.85 mins
BSTAR
0.00034086
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 18:34:19.026Z | 24.116° NE | 2026-06-22 18:37:19.026Z | 129.762° SE | 36.759° | 2026-06-22 18:39:19.026Z | 174.838° S |
| 4 mins | 2026-06-23 06:33:19.026Z | 222.659° SW | 2026-06-23 06:34:19.026Z | 250.229° W | 23.545° | 2026-06-23 06:37:19.026Z | 321.823° NNW |
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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