LEMUR 2 ALEX-MADDY, 44407 (Decayed)

Orbit data source: Space-Track

LEMUR 2 ALEX-MADDY, 44407 was a payload satellite owned by Spire (US) 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

LEMUR 2 ALEX-MADDY details

Identifier	44407, 2019-038X
Orbit	Decayed
Last TLE update	5 months ago
Origin	Spire (US)
Manufacturer	Spire/Glasgow
Mission	Decayed Commercial Com/MetRO
Bus & Motor	CUBESAT 3U, Unknown motor
Mass	4.6 kg wet, 4.6 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 + 2 Pan, 0.7 m
Radar Cross Section	0.124 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 5 months ago

0 LEMUR 2 ALEX-MADDY
1 44407U 19038X   24195.27284108  .14122455  27417-5  26926-3 0  9991
2 44407  97.6144 204.0152 0012814 244.2590 115.7390 16.46467790279136

Epoch: 2024-07-13T06:32Z

Definitive object data (Epoch: 2024-07-13T06:32:53.469Z)

Latitude	-0.00001°
Longitude	174.15527°
Altitude	155.549 km
Speed	7.811 km/s
True Right ascension	13h 36m 03s
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	153.822 km
Perigee altitude	137.103 km
Semi-major axis	6,523.6 km
Eccentricity	0.0012814
Inclination	97.6144°
RAAN	204.0152°
Arg. of periapsis	244.259°
True anomaly	115.87118°
Mean anomaly	115.739°
Eccentric anomaly	115.8051°
Mean motion	4.11919 °/min
BSTAR	0.00026926
Orbital period	87.4 mins