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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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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4Q 4
1 58327U 23174BZ 25303.17760071 .00027092 00000-0 73460-3 0 9997
2 58327 97.4029 22.4143 0006420 266.8748 93.1762 15.37586038110081Epoch: 2025-10-30T04:15Z
TLE epoch observation values (Epoch: 2025-10-30T04:15:44.701Z)
Latitude
-0.00003°
Longitude
-80.26208°
Altitude
456.61 km
Speed
7.638 km/s
True Right ascension
01h 29m 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
08:56:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
454.576 km
Perigee altitude
445.809 km
Semi-major axis
6,828.329 km
Eccentricity
0.00064
Inclination
97.4029°
RAAN
22.4143°
Arg. of periapsis
266.8748°
True anomaly
93.24965°
Mean anomaly
93.1762°
Eccentric anomaly
93.21293°
Mean motion
3.84655 °/min
Orbital period
93.59 mins
BSTAR
0.0007346
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-30 18:53:43.452Z | 326.617° NNW | 2025-10-30 18:54:43.452Z | 299.577° NW | 24.649° | 2025-10-30 18:57:43.452Z | 230.482° WSW |
| 5 mins | 2025-10-31 05:23:43.452Z | 159.806° S | 2025-10-31 05:25:43.452Z | 62.177° ENE | 44.199° | 2025-10-31 05:28:43.452Z | 351.543° N |
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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