Showing default

FLOCK 4Q 22, 58306

Orbit data source: Space-Track

FLOCK 4Q 22, 58306 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
58306, 2023-174BC
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: 19 hours ago

TLE from 19 hours ago
0 FLOCK 4Q 22
1 58306U 23174BC  26126.22340442  .00036156  00000-0  50764-3 0  9993
2 58306  97.3806 216.9685 0003617 275.1599  84.9243 15.56638272139333
Epoch: 2026-05-06T05:21Z
TLE epoch observation values (Epoch: 2026-05-06T05:21:42.141Z)
Latitude
-0.00006°
Longitude
-87.54406°
Altitude
400.319 km
Speed
7.67 km/s
True Right ascension
14h 27m 52s
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
08:28:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
396.76 km
Perigee altitude
391.861 km
Semi-major axis
6,772.448 km
Eccentricity
0.00036
Inclination
97.3806°
RAAN
216.9685°
Arg. of periapsis
275.1599°
True anomaly
84.96559°
Mean anomaly
84.9243°
Eccentric anomaly
84.94494°
Mean motion
3.89426 °/min
Orbital period
92.44 mins
BSTAR
0.00050764
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
|