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: 5 hours ago
TLE from 5 hours ago
0 FLOCK 4Q 2
1 58320U 23174BS 26126.84441016 .00019478 00000-0 37567-3 0 9990
2 58320 97.3822 214.3639 0004669 280.3390 79.7334 15.47867301139209Epoch: 2026-05-06T20:15Z
TLE epoch observation values (Epoch: 2026-05-06T20:15:57.037Z)
Latitude
-0.00003°
Longitude
45.67718°
Altitude
425.53 km
Speed
7.656 km/s
True Right ascension
14h 17m 27s
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
09:18:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
423.068 km
Perigee altitude
416.72 km
Semi-major axis
6,798.031 km
Eccentricity
0.00047
Inclination
97.3822°
RAAN
214.3639°
Arg. of periapsis
280.339°
True anomaly
79.78605°
Mean anomaly
79.7334°
Eccentric anomaly
79.75973°
Mean motion
3.8723 °/min
Orbital period
92.97 mins
BSTAR
0.00037567
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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 | 2026-05-07 05:42:28.283Z | 155.686° SSE | 2026-05-07 05:45:28.283Z | 30.071° NE | 39.043° | 2026-05-07 05:47:28.283Z | 356.797° N |
| 5 mins | 2026-05-07 18:33:28.283Z | 22.834° NE | 2026-05-07 18:35:28.283Z | 107.399° ESE | 42.214° | 2026-05-07 18:38:28.283Z | 183.723° SSW |
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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