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, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 FLOCK 4Q 27
1 58282U 23174AC 25258.18069413 .00032703 00000-0 87239-3 0 9993
2 58282 97.4062 338.2959 0007046 76.1520 284.0509 15.38048723103252Epoch: 2025-09-15T04:20Z
TLE epoch observation values (Epoch: 2025-09-15T04:20:11.972Z)
Latitude
0.00001°
Longitude
-81.14303°
Altitude
453.829 km
Speed
7.641 km/s
True Right ascension
22h 33m 11s
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
12:43:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.632 km
Perigee altitude
444.011 km
Semi-major axis
6,826.959 km
Eccentricity
0.0007
Inclination
97.4062°
RAAN
338.2959°
Arg. of periapsis
76.152°
True anomaly
283.97256°
Mean anomaly
284.0509°
Eccentric anomaly
284.01173°
Mean motion
3.84771 °/min
Orbital period
93.56 mins
BSTAR
0.00087239
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-16 05:27:01.039Z | 165.104° S | 2025-09-16 05:30:01.039Z | 358.672° N | 42.562° | 2025-09-16 05:32:01.039Z | 349.61° N |
| 5 mins | 2025-09-16 18:23:01.039Z | 7.126° NNE | 2025-09-16 18:25:01.039Z | 235.473° WSW | 43.978° | 2025-09-16 18:28:01.039Z | 196.655° SSW |
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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