FLOCK 4Q 25, 58303
Orbit data source: Space-Track
FLOCK 4Q 25, 58303 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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58303 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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4Q 25
1 58303U 23174AZ 25289.14593795 .00030477 00000-0 67936-3 0 9990
2 58303 97.4036 10.5180 0005325 296.0528 64.0171 15.43525078108088Epoch: 2025-10-16T03:30Z
TLE epoch observation values (Epoch: 2025-10-16T03:30:09.038Z)
Latitude
-0.00008°
Longitude
-66.9295°
Altitude
437.249 km
Speed
7.65 km/s
True Right ascension
00h 42m 04s
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
05:39:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
436.276 km
Perigee altitude
429.023 km
Semi-major axis
6,810.787 km
Eccentricity
0.00053
Inclination
97.4036°
RAAN
10.518°
Arg. of periapsis
296.0528°
True anomaly
64.07197°
Mean anomaly
64.0171°
Eccentric anomaly
64.04453°
Mean motion
3.86142 °/min
Orbital period
93.23 mins
BSTAR
0.00067936
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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 25 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 | 2025-10-16 18:03:58.998Z | 29.082° NE | 2025-10-16 18:06:58.998Z | 112.782° SE | 33.074° | 2025-10-16 18:08:58.998Z | 164.919° S |
| 4 mins | 2025-10-17 06:05:58.998Z | 219.278° SW | 2025-10-17 06:06:58.998Z | 249.728° W | 27.196° | 2025-10-17 06:09:58.998Z | 324.839° 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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