DECAYED
Showing default

FLOCK 4Y 23, 55080 (Decayed)

Orbit data source: Space-Track

FLOCK 4Y 23, 55080 was a payload satellite owned by Planet (US) in SSO that was launched on Tue, 03 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.

Not visible in the next 10 days
Identifier
55080, 2023-001BZ
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
Planet
Mission
Decayed Commercial Imaging
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5.7 kg wet, 5.7 kg dry
Launch date (UTC)
2023-01-03 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.108 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 5 months ago

TLE from 5 months ago
0 FLOCK 4Y 23
1 55080U 23001BZ  25170.70899041  .03070749  23884-5  20412-2 0  9998
2 55080  97.3474 247.0508 0014513 261.3909  98.5734 16.16761057137629
Epoch: 2025-06-19T17:00Z
TLE epoch observation values (Epoch: 2025-06-19T17:00:56.771Z)
Latitude
-0.00002°
Longitude
83.64147°
Altitude
233.026 km
Speed
7.766 km/s
True Right ascension
16h 28m 12s
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
09:17:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
234.78 km
Perigee altitude
215.613 km
Semi-major axis
6,603.333 km
Eccentricity
0.00145
Inclination
97.3474°
RAAN
247.0508°
Arg. of periapsis
261.3909°
True anomaly
98.7378°
Mean anomaly
98.5734°
Eccentric anomaly
98.65561°
Mean motion
4.04481 °/min
Orbital period
89 mins
BSTAR
0.0020412
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|