LUCKY-7, 44406 (Decayed)

Orbit data source: Space-Track

LUCKY-7, 44406 was a payload satellite owned by SkyFox Labs (CZ) in LEO that was launched on Fri, 05 Jul 2019 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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

LUCKY-7 details

Identifier	44406, 2019-038W
Orbit	Decayed
Last TLE update	1 week ago
Origin	SkyFox Labs (CZ / CZE)
Manufacturer	SkyFox Labs
Mission	Decayed Commercial Technology
Bus & Motor	CUBESAT 1U, Unknown motor
Mass	1 kg wet, 1 kg dry
Launch date (UTC)	2019-07-05 (5 years ago)
Launch vehicle	SOYUZ-2-1B
Launch site	Vostochny Cosmodrome (VOSTO)
Object type	Payload Rocket body Debris
Shape & HBR	Box, Unknown HBR
Radar Cross Section	0.015 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 1 week ago

0 LUCKY-7
1 44406U 19038W   24351.70569410  .16446325  26410-5  18169-3 0  9993
2 44406  97.6679   6.0836 0010327 352.1981   7.9160 16.50065787302877

Epoch: 2024-12-16T16:56Z

Definitive object data (Epoch: 2024-12-16T16:56:11.97Z)

Latitude	-0.00006°
Longitude	26.20896°
Altitude	135.751 km
Speed	7.829 km/s
True Right ascension	00h 24m 20s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	142.696 km
Perigee altitude	129.242 km
Semi-major axis	6,514.106 km
Eccentricity	0.0010327
Inclination	97.6679°
RAAN	6.0836°
Arg. of periapsis	352.1981°
True anomaly	7.93232°
Mean anomaly	7.916°
Eccentric anomaly	7.92416°
Mean motion	4.1282 °/min
BSTAR	0.00018169
Orbital period	87.21 mins