Showing default

ELEKTRO-L 4, 55506

Orbit data source: Space-Track

ELEKTRO-L 4, 55506 is a Commonwealth of Independent States-origin payload satellite in GEO that was launched on Sun, 05 Feb 2023 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

Identifier	55506, 2023-016A
Orbit	GEO
Last TLE update	1 day 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)	2023-02-05 (2 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, 10 m
Radar Cross Section	11.105 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 ELEKTRO-L 4
1 55506U 23016A   25072.06466169 -.00000071  00000-0  00000-0 0  9996
2 55506   0.0467 343.7375 0000561 347.7466  28.4831  1.00271669  7703

Epoch: 2025-03-13T01:33Z

Definitive object data (Epoch: 2025-03-13T01:33:06.77Z)

Latitude	-0.00992°
Longitude	165.77749°
Altitude	35,784.029 km
Speed	3.075 km/s
True Right ascension	23h 59m 59s
True Declination	0° 00' 36"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-0.01823°
Longitude	-118.42114°
Altitude	35,786.678 km
Speed	3.075 km/s
Apparent Right ascension	04h 36m 39s
Apparent Declination	-5° 30' 21"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	10:59:37
Azimuth	269.44° W
Elevation	-7.93°
Doppler factor	1

Orbital elements

Apogee altitude	35,790.063 km
Perigee altitude	35,785.332 km
Semi-major axis	42,165.835 km
Eccentricity	0.0000561
Inclination	0.0467°
RAAN	343.7375°
Arg. of periapsis	347.7466°
True anomaly	28.48617°
Mean anomaly	28.4831°
Eccentric anomaly	28.48463°
Mean motion	0.25067 °/min
BSTAR	Unknown
Orbital period	1436.15 mins