FLOCK 4Q 17, 58283
Orbit data source: Space-Track
FLOCK 4Q 17, 58283 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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58283 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: 13 hours ago
TLE from 13 hours ago
0 FLOCK 4Q 17
1 58283U 23174AD 25365.19780080 .00062821 00000-0 10140-2 0 9994
2 58283 97.3966 89.2251 0005417 36.5143 323.6479 15.52671397119904Epoch: 2025-12-31T04:44Z
TLE epoch observation values (Epoch: 2025-12-31T04:44:49.989Z)
Latitude
0.00007°
Longitude
-81.85337°
Altitude
409.104 km
Speed
7.667 km/s
True Right ascension
05h 56m 54s
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
17:31:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
409.527 km
Perigee altitude
402.177 km
Semi-major axis
6,783.989 km
Eccentricity
0.00054
Inclination
97.3966°
RAAN
89.2251°
Arg. of periapsis
36.5143°
True anomaly
323.61109°
Mean anomaly
323.6479°
Eccentric anomaly
323.62949°
Mean motion
3.88432 °/min
Orbital period
92.68 mins
BSTAR
0.001014
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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 17 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-31 19:13:16.509Z | 343.527° N | 2025-12-31 19:15:16.509Z | 298.831° NW | 24.135° | 2025-12-31 19:17:16.509Z | 240.434° WSW |
| 4 mins | 2026-01-01 05:38:16.509Z | 146.733° SSE | 2026-01-01 05:40:16.509Z | 63.427° ENE | 38.71° | 2026-01-01 05:42:16.509Z | 2.12° NNE |
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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