DECAYED
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FLOCK 4Y 10, 55029 (Decayed)

Orbit data source: Space-Track

FLOCK 4Y 10, 55029 was a payload satellite owned by Planet (US) in LEO 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
55029, 2023-001W
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: 1 month ago

TLE from 1 month ago
0 FLOCK 4Y 10
1 55029U 23001W   25259.89579816  .05373729  24341-5  14748-2 0  9994
2 55029  97.3268 338.3052 0013234 276.5500  83.4286 16.27809707151454
Epoch: 2025-09-16T21:29Z
TLE epoch observation values (Epoch: 2025-09-16T21:29:56.961Z)
Latitude
-0.00004°
Longitude
19.73834°
Altitude
200.685 km
Speed
7.786 km/s
True Right ascension
22h 33m 13s
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
12:47:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
203.952 km
Perigee altitude
186.554 km
Semi-major axis
6,573.39 km
Eccentricity
0.00132
Inclination
97.3268°
RAAN
338.3052°
Arg. of periapsis
276.55°
True anomaly
83.57928°
Mean anomaly
83.4286°
Eccentric anomaly
83.50394°
Mean motion
4.07248 °/min
Orbital period
88.4 mins
BSTAR
0.0014748
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Computing Atmospheric mass density...

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