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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4Q 27
1 58282U 23174AC 26023.94440963 .00041974 00000-0 86050-3 0 9991
2 58282 97.3921 110.9164 0004763 307.3017 52.7797 15.45934661123402Epoch: 2026-01-23T22:39Z
TLE epoch observation values (Epoch: 2026-01-23T22:39:56.992Z)
Latitude
-0.00005°
Longitude
7.65298°
Altitude
429.798 km
Speed
7.655 km/s
True Right ascension
07h 23m 39s
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
07:33:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
428.804 km
Perigee altitude
422.323 km
Semi-major axis
6,803.701 km
Eccentricity
0.00048
Inclination
97.3921°
RAAN
110.9164°
Arg. of periapsis
307.3017°
True anomaly
52.82318°
Mean anomaly
52.7797°
Eccentric anomaly
52.80144°
Mean motion
3.86746 °/min
Orbital period
93.08 mins
BSTAR
0.0008605
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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 | 2026-01-24 17:53:23.088Z | 58.663° ENE | 2026-01-24 17:55:23.088Z | 109.5° ESE | 19.669° | 2026-01-24 17:57:23.088Z | 147.525° SSE |
| 5 mins | 2026-01-25 05:52:23.088Z | 179.581° S | 2026-01-25 05:54:23.088Z | 260.253° W | 42.642° | 2026-01-25 05:57:23.088Z | 342.06° N |
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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