FLOCK 4Q 27, 58282
Orbit data source: Space-Track
FLOCK 4Q 27, 58282 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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58282 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: 22 hours ago
TLE from 22 hours ago
0 FLOCK 4Q 27
1 58282U 23174AC 25288.22161381 .00024828 00000-0 62648-3 0 9994
2 58282 97.4040 8.6413 0005067 314.0458 46.0370 15.39826738107871Epoch: 2025-10-15T05:19Z
TLE epoch observation values (Epoch: 2025-10-15T05:19:07.433Z)
Latitude
-0°
Longitude
-95.13847°
Altitude
447.338 km
Speed
7.645 km/s
True Right ascension
00h 34m 33s
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
22:06:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.017 km
Perigee altitude
440.104 km
Semi-major axis
6,821.698 km
Eccentricity
0.00051
Inclination
97.404°
RAAN
8.6413°
Arg. of periapsis
314.0458°
True anomaly
46.07881°
Mean anomaly
46.037°
Eccentric anomaly
46.0579°
Mean motion
3.85216 °/min
Orbital period
93.45 mins
BSTAR
0.00062648
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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 27 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 | 2025-10-16 04:51:42.401Z | 117.59° SE | 2025-10-16 04:53:42.401Z | 72.556° E | 21.618° | 2025-10-16 04:55:42.401Z | 25.942° NE |
| 4 mins | 2025-10-16 17:46:42.401Z | 61.505° ENE | 2025-10-16 17:47:42.401Z | 88.852° E | 23.561° | 2025-10-16 17:50:42.401Z | 154.619° SSE |
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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