FLOCK 4Q 12, 58275
Orbit data source: Space-Track
FLOCK 4Q 12, 58275 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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58275 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: 5 hours ago
TLE from 5 hours ago
0 FLOCK 4Q 12
1 58275U 23174V 25290.19994971 .00032222 00000-0 76770-3 0 9992
2 58275 97.4060 11.4340 0005654 310.9088 49.1669 15.41514423108225Epoch: 2025-10-17T04:47Z
TLE epoch observation values (Epoch: 2025-10-17T04:47:55.654Z)
Latitude
-0.00001°
Longitude
-86.49663°
Altitude
442.238 km
Speed
7.648 km/s
True Right ascension
00h 45m 44s
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
04:37:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
442.43 km
Perigee altitude
434.722 km
Semi-major axis
6,816.713 km
Eccentricity
0.00057
Inclination
97.406°
RAAN
11.434°
Arg. of periapsis
310.9088°
True anomaly
49.21594°
Mean anomaly
49.1669°
Eccentric anomaly
49.19142°
Mean motion
3.85639 °/min
Orbital period
93.35 mins
BSTAR
0.0007677
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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 12 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 | 2025-10-17 17:50:07.171Z | 45.142° ENE | 2025-10-17 17:52:07.171Z | 91.909° ESE | 24.116° | 2025-10-17 17:55:07.171Z | 156.458° SSE |
| 4 mins | 2025-10-18 05:52:07.171Z | 195.215° SSW | 2025-10-18 05:54:07.171Z | 283.473° WNW | 36.327° | 2025-10-18 05:56:07.171Z | 331.971° NNW |
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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