FLOCK 4Q 26, 58284
Orbit data source: Space-Track
FLOCK 4Q 26, 58284 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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58284 intel report (Beta)
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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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4Q 26
1 58284U 23174AE 26126.79179918 .00029691 00000-0 44825-3 0 9995
2 58284 97.3867 217.8511 0004830 293.2349 66.8396 15.54689908139399Epoch: 2026-05-06T19:00Z
TLE epoch observation values (Epoch: 2026-05-06T19:00:11.449Z)
Latitude
-0.00001°
Longitude
68.15618°
Altitude
404.905 km
Speed
7.668 km/s
True Right ascension
14h 31m 24s
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
09:18:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
403.247 km
Perigee altitude
396.699 km
Semi-major axis
6,778.11 km
Eccentricity
0.00048
Inclination
97.3867°
RAAN
217.8511°
Arg. of periapsis
293.2349°
True anomaly
66.8905°
Mean anomaly
66.8396°
Eccentric anomaly
66.86505°
Mean motion
3.88938 °/min
Orbital period
92.56 mins
BSTAR
0.00044825
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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 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 | 2026-05-07 05:56:43.536Z | 156.62° SSE | 2026-05-07 05:59:43.536Z | 41.526° NE | 40.396° | 2026-05-07 06:01:43.536Z | 357.218° N |
| 4 mins | 2026-05-07 18:44:43.536Z | 28.167° NE | 2026-05-07 18:46:43.536Z | 122.858° SE | 39.108° | 2026-05-07 18:48:43.536Z | 176.593° S |
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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