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: 14 hours ago
TLE from 14 hours ago
0 FLOCK 4Q 31
1 58285U 23174AF 25358.75745632 .00027576 00000-0 58607-3 0 9993
2 58285 97.4060 81.0354 0007658 71.1205 289.0873 15.44942932118740Epoch: 2025-12-24T18:10Z
TLE epoch observation values (Epoch: 2025-12-24T18:10:44.226Z)
Latitude
-0.00003°
Longitude
74.82886°
Altitude
432.968 km
Speed
7.653 km/s
True Right ascension
05h 24m 08s
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
06:57:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
433.691 km
Perigee altitude
423.266 km
Semi-major axis
6,806.615 km
Eccentricity
0.00077
Inclination
97.406°
RAAN
81.0354°
Arg. of periapsis
71.1205°
True anomaly
289.00434°
Mean anomaly
289.0873°
Eccentric anomaly
289.04582°
Mean motion
3.86497 °/min
Orbital period
93.14 mins
BSTAR
0.00058607
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-25 18:03:50.709Z | 39.765° NE | 2025-12-25 18:05:50.709Z | 87.522° E | 26.863° | 2025-12-25 18:08:50.709Z | 160.727° S |
| 4 mins | 2025-12-26 06:04:50.709Z | 209.585° SW | 2025-12-26 06:05:50.709Z | 248.388° W | 33.462° | 2025-12-26 06:08:50.709Z | 331.899° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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