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FLOCK 4Y 28, 55033

Orbit data source: Space-Track

FLOCK 4Y 28, 55033 is 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). Payloads include a variety of satellites, spacecraft, and rockets 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

FLOCK 4Y 28 details

Identifier	55033, 2023-001AA
Orbit	SSO
Last TLE update	4 hours ago
Origin	Planet (US)
Manufacturer	Planet
Mission	Non-operational Commercial Imaging
Bus & Motor	CUBESAT 3U, Unknown motor
Mass	5.7 kg wet, 5.7 kg dry
Launch date (UTC)	2023-01-03 (2 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, 0.3 m
Radar Cross Section	0.108 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 4 hours ago

0 FLOCK 4Y 28
1 55033U 23001AA  25036.19707090  .01459609  13062-2  22899-2 0  9991
2 55033  97.3697 112.9543 0007140 301.3490  58.7091 16.04251887117063

Epoch: 2025-02-05T04:43Z

Definitive object data (Epoch: 2025-02-05T04:43:46.925Z)

Latitude	-0.00007°
Longitude	-93.58268°
Altitude	263.403 km
Speed	7.75 km/s
True Right ascension	07h 31m 49s
True Declination	0° 00' 00"
Sunlit	Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude	-33.4059°
Longitude	81.7309°
Altitude	273.72 km
Speed	7.742 km/s
Apparent Right ascension	20h 49m 09s
Apparent Declination	-39° 18' 19"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	10:39:11
Azimuth	97.251° ESE
Elevation	-68.883°
Doppler factor	1

Orbital elements

Apogee altitude	264.251 km
Perigee altitude	254.773 km
Semi-major axis	6,637.649 km
Eccentricity	0.000714
Inclination	97.3697°
RAAN	112.9543°
Arg. of periapsis	301.349°
True anomaly	58.77905°
Mean anomaly	58.7091°
Eccentric anomaly	58.74407°
Mean motion	4.01349 °/min
BSTAR	0.0022899
Orbital period	89.7 mins