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ELEKTRO-L 3, 44903

Orbit data source: Space-Track

ELEKTRO-L 3, 44903 is a Commonwealth of Independent States-origin payload satellite in GEO that was launched on Tue, 24 Dec 2019 UTC via a PROTON-M/DM-3 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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

ELEKTRO-L 3 details

Identifier	44903, 2019-095A
Orbit	GEO
Last TLE update	9 hours ago
Origin	RGMS/NPOLO (CIS)
Manufacturer	Lavochkin
Mission	Operational Civil Weather
Bus & Motor	NAVIGATOR, Unknown motor
Mass	2,283 kg wet, 1,589 kg dry
Launch date (UTC)	2019-12-24 (5 years ago)
Launch vehicle	PROTON-M/DM-3
Launch site	Tyuratam Missile And Space Complex (TTMTR)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 1 Pan + 1 Ant, Unknown HBR
Radar Cross Section	11.105 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 9 hours ago

0 ELEKTRO-L 3
1 44903U 19095A   24361.54457226 -.00000068  00000-0  00000-0 0  9990
2 44903   0.0525 165.9942 0002003 124.0642  77.5580  1.00271637 18316

Epoch: 2024-12-26T13:04Z

Definitive object data (Epoch: 2024-12-26T13:04:11.043Z)

Latitude	-0.02331°
Longitude	76.06266°
Altitude	35,784.33 km
Speed	3.075 km/s
True Right ascension	00h 30m 31s
True Declination	0° 01' 24"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	0.00342°
Longitude	-154.87792°
Altitude	35,793.692 km
Speed	3.074 km/s
Apparent Right ascension	09h 06m 17s
Apparent Declination	-4° 56' 24"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	21:02:10
Azimuth	358.213° N
Elevation	-55.012°
Doppler factor	1

Orbital elements

Apogee altitude	35,796.153 km
Perigee altitude	35,779.261 km
Semi-major axis	42,165.844 km
Eccentricity	0.0002003
Inclination	0.0525°
RAAN	165.9942°
Arg. of periapsis	124.0642°
True anomaly	77.58041°
Mean anomaly	77.558°
Eccentric anomaly	77.56921°
Mean motion	0.25067 °/min
BSTAR	Unknown
Orbital period	1436.15 mins