FLOCK 4Q 30, 58286
Orbit data source: Space-Track
FLOCK 4Q 30, 58286 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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58286 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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4Q 30
1 58286U 23174AG 25291.17422827 .00031135 00000-0 76482-3 0 9991
2 58286 97.4131 12.4699 0006604 301.5797 58.4804 15.40589400108335Epoch: 2025-10-18T04:10Z
TLE epoch observation values (Epoch: 2025-10-18T04:10:53.322Z)
Latitude
-0.00004°
Longitude
-77.1613°
Altitude
445.133 km
Speed
7.646 km/s
True Right ascension
00h 49m 52s
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
16:11:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
445.811 km
Perigee altitude
436.804 km
Semi-major axis
6,819.444 km
Eccentricity
0.00066
Inclination
97.4131°
RAAN
12.4699°
Arg. of periapsis
301.5797°
True anomaly
58.54494°
Mean anomaly
58.4804°
Eccentric anomaly
58.51267°
Mean motion
3.85407 °/min
Orbital period
93.41 mins
BSTAR
0.00076482
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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 30 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-19 05:14:57.708Z | 146.849° SSE | 2025-10-19 05:17:57.708Z | 79.17° E | 34.804° | 2025-10-19 05:20:57.708Z | 2.828° NNE |
| 5 mins | 2025-10-19 18:09:57.708Z | 30.252° NE | 2025-10-19 18:11:57.708Z | 96.466° ESE | 37.78° | 2025-10-19 18:14:57.708Z | 175.884° 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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