FLOCK 4Q 28, 58280
Orbit data source: Space-Track
FLOCK 4Q 28, 58280 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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58280 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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4Q 28
1 58280U 23174AA 25341.20261200 .00036461 00000-0 82116-3 0 9999
2 58280 97.4050 62.7186 0007662 127.3435 232.8512 15.43165021116027Epoch: 2025-12-07T04:51Z
TLE epoch observation values (Epoch: 2025-12-07T04:51:45.676Z)
Latitude
-0.00002°
Longitude
-86.44109°
Altitude
443.053 km
Speed
7.644 km/s
True Right ascension
04h 10m 52s
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
20:01:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
438.929 km
Perigee altitude
428.491 km
Semi-major axis
6,811.847 km
Eccentricity
0.00077
Inclination
97.405°
RAAN
62.7186°
Arg. of periapsis
127.3435°
True anomaly
232.78126°
Mean anomaly
232.8512°
Eccentric anomaly
232.81622°
Mean motion
3.86052 °/min
Orbital period
93.25 mins
BSTAR
0.00082116
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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 28 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 | 2025-12-08 05:53:32.716Z | 185.072° SSW | 2025-12-08 05:55:32.716Z | 225.379° WSW | 36.355° | 2025-12-08 05:58:32.716Z | 334.871° NNW |
| 5 mins | 2025-12-08 18:46:32.716Z | 353.678° N | 2025-12-08 18:48:32.716Z | 293.098° NW | 36.408° | 2025-12-08 18:51:32.716Z | 211.343° SW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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