FLOCK 4Q 31, 58285
Orbit data source: Space-Track
FLOCK 4Q 31, 58285 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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58285 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: 12 hours ago
TLE from 12 hours ago
0 FLOCK 4Q 31
1 58285U 23174AF 25298.77122276 .00028690 00000-0 69609-3 0 9993
2 58285 97.4118 20.0289 0007172 275.4342 84.6086 15.40978719109491Epoch: 2025-10-25T18:30Z
TLE epoch observation values (Epoch: 2025-10-25T18:30:33.646Z)
Latitude
-0.00004°
Longitude
67.99172°
Altitude
445.882 km
Speed
7.645 km/s
True Right ascension
01h 20m 06s
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
01:25:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
445.048 km
Perigee altitude
435.268 km
Semi-major axis
6,818.295 km
Eccentricity
0.00072
Inclination
97.4118°
RAAN
20.0289°
Arg. of periapsis
275.4342°
True anomaly
84.69043°
Mean anomaly
84.6086°
Eccentric anomaly
84.64951°
Mean motion
3.85505 °/min
Orbital period
93.38 mins
BSTAR
0.00069609
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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 31 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-26 18:26:08.830Z | 10.961° NNE | 2025-10-26 18:29:08.830Z | 359.007° N | 43.804° | 2025-10-26 18:32:08.830Z | 194.485° SSW |
| 4 mins | 2025-10-27 04:57:08.830Z | 109.622° ESE | 2025-10-27 04:59:08.830Z | 56.7° ENE | 21.41° | 2025-10-27 05:01:08.830Z | 18.517° NNE |
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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