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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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: 10 hours ago
TLE from 10 hours ago
0 FLOCK 4Q 27
1 58282U 23174AC 26080.76860655 .00040805 00000-0 73257-3 0 9995
2 58282 97.3829 168.9740 0006812 113.4166 246.7802 15.49763433132199Epoch: 2026-03-21T18:26Z
TLE epoch observation values (Epoch: 2026-03-21T18:26:47.605Z)
Latitude
-0.00007°
Longitude
72.99108°
Altitude
422.377 km
Speed
7.657 km/s
True Right ascension
11h 15m 53s
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
09:37:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
418.97 km
Perigee altitude
409.716 km
Semi-major axis
6,792.48 km
Eccentricity
0.00068
Inclination
97.3829°
RAAN
168.974°
Arg. of periapsis
113.4166°
True anomaly
246.70849°
Mean anomaly
246.7802°
Eccentric anomaly
246.74434°
Mean motion
3.87704 °/min
Orbital period
92.85 mins
BSTAR
0.00073257
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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 | 2026-03-22 05:26:25.293Z | 130.16° SE | 2026-03-22 05:28:25.293Z | 69.642° E | 29.16° | 2026-03-22 05:30:25.293Z | 14.545° NNE |
| 4 mins | 2026-03-22 18:16:25.293Z | 53.649° ENE | 2026-03-22 18:17:25.293Z | 86.736° E | 28.179° | 2026-03-22 18:20:25.293Z | 163.62° S |
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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