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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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: 15 hours ago
TLE from 15 hours ago
0 FLOCK 4Q 26
1 58284U 23174AE 25291.26381957 .00035264 00000-0 84512-3 0 9997
2 58284 97.4094 12.7122 0006306 306.1276 53.9386 15.41314497108379Epoch: 2025-10-18T06:19Z
TLE epoch observation values (Epoch: 2025-10-18T06:19:54.010Z)
Latitude
-0.0001°
Longitude
-109.26017°
Altitude
442.817 km
Speed
7.648 km/s
True Right ascension
00h 50m 50s
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
16:11:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
443.465 km
Perigee altitude
434.867 km
Semi-major axis
6,817.303 km
Eccentricity
0.00063
Inclination
97.4094°
RAAN
12.7122°
Arg. of periapsis
306.1276°
True anomaly
53.99704°
Mean anomaly
53.9386°
Eccentric anomaly
53.96782°
Mean motion
3.85589 °/min
Orbital period
93.36 mins
BSTAR
0.00084512
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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 | 2025-10-19 05:49:56.763Z | 184.298° SSW | 2025-10-19 05:52:56.763Z | 294.149° NW | 36.88° | 2025-10-19 05:54:56.763Z | 334.822° NNW |
| 5 mins | 2025-10-19 18:43:56.763Z | 353.338° N | 2025-10-19 18:45:56.763Z | 294.824° NW | 36.316° | 2025-10-19 18:48:56.763Z | 212.163° SW |
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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