Showing default

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.

Loading next visibility...
Identifier
58280, 2023-174AA
Orbit
SSO
Country
Flag of USUS
Related 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)
2023-11-11 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 FLOCK 4Q 28
1 58280U 23174AA  25291.21980904  .00031979  00000-0  80218-3 0  9993
2 58280  97.4097  12.0144 0005859 305.7106  54.3594 15.39950881108325
Epoch: 2025-10-18T05:16Z
TLE epoch observation values (Epoch: 2025-10-18T05:16:31.501Z)
Latitude
-0.00002°
Longitude
-94.07081°
Altitude
447.043 km
Speed
7.645 km/s
True Right ascension
00h 48m 03s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
16:11:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.19 km
Perigee altitude
439.197 km
Semi-major axis
6,821.331 km
Eccentricity
0.00059
Inclination
97.4097°
RAAN
12.0144°
Arg. of periapsis
305.7106°
True anomaly
54.41399°
Mean anomaly
54.3594°
Eccentric anomaly
54.38669°
Mean motion
3.85247 °/min
Orbital period
93.45 mins
BSTAR
0.00080218
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|