FLOCK 4Q 23, 58307
Orbit data source: Space-Track
FLOCK 4Q 23, 58307 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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58307 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: 1 day ago
TLE from 1 day ago
0 FLOCK 4Q 23
1 58307U 23174BD 25315.20786657 .00043835 00000-0 93887-3 0 9998
2 58307 97.4107 37.5642 0007429 203.2070 156.8844 15.44619265112087Epoch: 2025-11-11T04:59Z
TLE epoch observation values (Epoch: 2025-11-11T04:59:19.671Z)
Latitude
-0.00004°
Longitude
-87.86548°
Altitude
440.276 km
Speed
7.645 km/s
True Right ascension
02h 30m 15s
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
02:08:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
434.488 km
Perigee altitude
424.373 km
Semi-major axis
6,807.567 km
Eccentricity
0.00074
Inclination
97.4107°
RAAN
37.5642°
Arg. of periapsis
203.207°
True anomaly
156.91779°
Mean anomaly
156.8844°
Eccentric anomaly
156.9011°
Mean motion
3.86416 °/min
Orbital period
93.16 mins
BSTAR
0.00093887
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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 23 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 | 2025-11-12 05:59:27.065Z | 188.545° SSW | 2025-11-12 06:02:27.065Z | 279.241° WNW | 34.642° | 2025-11-12 06:04:27.065Z | 329.513° NNW |
| 4 mins | 2025-11-12 18:52:27.065Z | 344.179° N | 2025-11-12 18:54:27.065Z | 264.932° W | 32.714° | 2025-11-12 18:56:27.065Z | 218.544° SW |
| 4 mins | 2025-11-13 05:20:27.065Z | 125.528° SE | 2025-11-13 05:21:27.065Z | 91.465° ESE | 32.282° | 2025-11-13 05:24:27.065Z | 5.853° 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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