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, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 FLOCK 4Q 30
1 58286U 23174AG 25260.69191893 .00020369 00000-0 53603-3 0 9997
2 58286 97.4157 341.6113 0008374 65.9542 294.2579 15.38553945103646Epoch: 2025-09-17T16:36Z
TLE epoch observation values (Epoch: 2025-09-17T16:36:21.795Z)
Latitude
0.00001°
Longitude
95.65626°
Altitude
451.154 km
Speed
7.643 km/s
True Right ascension
22h 46m 26s
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
01:25:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.042 km
Perigee altitude
441.611 km
Semi-major axis
6,825.463 km
Eccentricity
0.00084
Inclination
97.4157°
RAAN
341.6113°
Arg. of periapsis
65.9542°
True anomaly
294.17038°
Mean anomaly
294.2579°
Eccentric anomaly
294.21414°
Mean motion
3.84897 °/min
Orbital period
93.53 mins
BSTAR
0.00053603
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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 | 2025-09-18 18:08:12.785Z | 21.934° NNE | 2025-09-18 18:11:12.785Z | 100.256° ESE | 39.614° | 2025-09-18 18:14:12.785Z | 178.725° 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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