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: 20 hours ago
TLE from 20 hours ago
0 FLOCK 4Q 30
1 58286U 23174AG 25302.47308271 .00032709 00000-0 78382-3 0 9992
2 58286 97.4110 23.9296 0007124 255.3546 104.6911 15.41327255110074Epoch: 2025-10-29T11:21Z
TLE epoch observation values (Epoch: 2025-10-29T11:21:14.346Z)
Latitude
-0.00001°
Longitude
175.57411°
Altitude
446.546 km
Speed
7.644 km/s
True Right ascension
01h 35m 43s
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
03:12:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
443.985 km
Perigee altitude
434.272 km
Semi-major axis
6,817.266 km
Eccentricity
0.00071
Inclination
97.411°
RAAN
23.9296°
Arg. of periapsis
255.3546°
True anomaly
104.77005°
Mean anomaly
104.6911°
Eccentric anomaly
104.73058°
Mean motion
3.85592 °/min
Orbital period
93.36 mins
BSTAR
0.00078382
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-30 19:05:23.975Z | 324.321° NNW | 2025-10-30 19:06:23.975Z | 298.05° NW | 22.777° | 2025-10-30 19:09:23.975Z | 232.342° WSW |
| 4 mins | 2025-10-31 05:34:23.975Z | 159.711° S | 2025-10-31 05:35:23.975Z | 142.5° SSE | 42.572° | 2025-10-31 05:38:23.975Z | 351.112° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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