FLOCK 4Q 4, 58327
Orbit data source: Space-Track
FLOCK 4Q 4, 58327 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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58327 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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4Q 4
1 58327U 23174BZ 26263.52373726 .00021176 00000-0 34453-3 0 9995
2 58327 97.3776 353.6007 0005297 167.8346 192.3036 15.52681354160335Epoch: 2026-09-20T12:34Z
TLE epoch observation values (Epoch: 2026-09-20T12:34:10.899Z)
Latitude
0.00001°
Longitude
165.6386°
Altitude
415.55 km
Speed
7.66 km/s
True Right ascension
23h 34m 24s
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
15:02:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
409.416 km
Perigee altitude
402.229 km
Semi-major axis
6,783.959 km
Eccentricity
0.00053
Inclination
97.3776°
RAAN
353.6007°
Arg. of periapsis
167.8346°
True anomaly
192.29067°
Mean anomaly
192.3036°
Eccentric anomaly
192.29714°
Mean motion
3.88435 °/min
Orbital period
92.68 mins
BSTAR
0.00034453
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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 4 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 | 2026-09-21 05:43:28.704Z | 133.013° SE | 2026-09-21 05:45:28.704Z | 82.831° E | 32.662° | 2026-09-21 05:48:28.704Z | 8.322° NNE |
| 4 mins | 2026-09-21 18:32:28.704Z | 56.878° ENE | 2026-09-21 18:33:28.704Z | 89.802° E | 30.377° | 2026-09-21 18:36:28.704Z | 162.266° S |
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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