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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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: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4Q 30
1 58286U 23174AG 26080.81357372 .00049394 00000-0 83190-3 0 9991
2 58286 97.3947 170.3266 0006750 115.7915 244.4034 15.51530801132222Epoch: 2026-03-21T19:31Z
TLE epoch observation values (Epoch: 2026-03-21T19:31:32.769Z)
Latitude
-0.00005°
Longitude
58.11117°
Altitude
417.372 km
Speed
7.66 km/s
True Right ascension
11h 21m 18s
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
11:05:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
413.761 km
Perigee altitude
404.598 km
Semi-major axis
6,787.316 km
Eccentricity
0.00068
Inclination
97.3947°
RAAN
170.3266°
Arg. of periapsis
115.7915°
True anomaly
244.33367°
Mean anomaly
244.4034°
Eccentric anomaly
244.36853°
Mean motion
3.88147 °/min
Orbital period
92.75 mins
BSTAR
0.0008319
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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 | 2026-03-22 06:29:49.160Z | 211.308° SW | 2026-03-22 06:31:49.160Z | 265.503° W | 24.639° | 2026-03-22 06:33:49.160Z | 316.19° NNW |
| 4 mins | 2026-03-22 19:18:49.160Z | 330.108° NNW | 2026-03-22 19:19:49.160Z | 301.027° NW | 25.168° | 2026-03-22 19:22:49.160Z | 226.412° WSW |
| 4 mins | 2026-03-23 05:43:49.160Z | 137.92° SSE | 2026-03-23 05:44:49.160Z | 102.948° ESE | 36.344° | 2026-03-23 05:47:49.160Z | 0.517° NNE |
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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