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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4Q 17
1 58283U 23174AD 25291.23333567 .00047911 00000-0 99593-3 0 9994
2 58283 97.4041 13.4095 0005309 297.9784 62.0928 15.45495096108451Epoch: 2025-10-18T05:36Z
TLE epoch observation values (Epoch: 2025-10-18T05:36:00.201Z)
Latitude
0.00002°
Longitude
-97.55863°
Altitude
431.358 km
Speed
7.654 km/s
True Right ascension
00h 53m 38s
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
07:37:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
430.468 km
Perigee altitude
423.243 km
Semi-major axis
6,804.993 km
Eccentricity
0.00053
Inclination
97.4041°
RAAN
13.4095°
Arg. of periapsis
297.9784°
True anomaly
62.14658°
Mean anomaly
62.0928°
Eccentric anomaly
62.11969°
Mean motion
3.86635 °/min
Orbital period
93.11 mins
BSTAR
0.00099593
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-18 18:34:49.901Z | 7.102° NNE | 2025-10-18 18:37:49.901Z | 304.593° NW | 43.115° | 2025-10-18 18:40:49.901Z | 200.344° SSW |
| 4 mins | 2025-10-19 05:03:49.901Z | 113.32° SE | 2025-10-19 05:05:49.901Z | 56.729° ENE | 22.661° | 2025-10-19 05:07:49.901Z | 16.857° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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