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: 12 hours ago
TLE from 12 hours ago
0 FLOCK 4Q 4
1 58327U 23174BZ 26126.50884837 .00018078 00000-0 36017-3 0 9996
2 58327 97.3816 213.3580 0004383 314.5427 45.5465 15.46942716139116Epoch: 2026-05-06T12:12Z
TLE epoch observation values (Epoch: 2026-05-06T12:12:44.499Z)
Latitude
0.00006°
Longitude
165.80425°
Altitude
426.715 km
Speed
7.657 km/s
True Right ascension
14h 13m 25s
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
08:29:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
425.585 km
Perigee altitude
419.624 km
Semi-major axis
6,800.742 km
Eccentricity
0.00044
Inclination
97.3816°
RAAN
213.358°
Arg. of periapsis
314.5427°
True anomaly
45.58237°
Mean anomaly
45.5465°
Eccentric anomaly
45.56443°
Mean motion
3.86998 °/min
Orbital period
93.02 mins
BSTAR
0.00036017
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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 | 2026-05-07 05:25:16.286Z | 141.35° SSE | 2026-05-07 05:28:16.286Z | 62.52° ENE | 31.037° | 2026-05-07 05:30:16.286Z | 11.01° NNE |
| 4 mins | 2026-05-07 18:17:16.286Z | 43.419° NE | 2026-05-07 18:19:16.286Z | 119.748° SE | 30.92° | 2026-05-07 18:21:16.286Z | 164.903° 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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