FLOCK 4Q 26, 58284 (Decayed)
Orbit data source: Space-Track
FLOCK 4Q 26, 58284 was a payload satellite owned by Planet (US) in LEO 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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58284 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Decayed 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 month ago
TLE from 1 month ago
0 FLOCK 4Q 26
1 58284U 23174AE 26245.00021628 .17429963 25254-5 38180-3 0 9999
2 58284 97.3586 342.2178 0007949 277.5642 82.4757 16.46255717157916Epoch: 2026-09-02T00:00Z
TLE epoch observation values (Epoch: 2026-09-02T00:00:18.686Z)
Latitude
-0.00011°
Longitude
0.98092°
Altitude
151.799 km
Speed
7.815 km/s
True Right ascension
22h 48m 52s
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
03:25:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
151.198 km
Perigee altitude
140.826 km
Semi-major axis
6,524.149 km
Eccentricity
0.00079
Inclination
97.3586°
RAAN
342.2178°
Arg. of periapsis
277.5642°
True anomaly
82.56602°
Mean anomaly
82.4757°
Eccentric anomaly
82.52086°
Mean motion
4.11867 °/min
Orbital period
87.41 mins
BSTAR
0.0003818
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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 26 Visibility
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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. |
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| This satellite is decayed. |
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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