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). Payload-class satellites include a variety of spacecraft 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.
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55506 intel report (Beta)
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ELEKTRO-L 4 radio frequencies
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Lavochkin
Mission
Operational Civil Weather
Bus & Motor
NAVIGATOR, Unknown motor
Mass
2,283 kg wet, 1,589 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan + 1 Ant, 5.0 m
Radar Cross Section
11.105 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ELEKTRO-L 4
1 55506U 23016A 25260.54852372 -.00000079 00000-0 00000-0 0 9991
2 55506 0.0578 351.7333 0002227 227.1945 141.0544 1.00270978 9609Epoch: 2025-09-17T13:09Z
TLE epoch observation values (Epoch: 2025-09-17T13:09:52.449Z)
Latitude
-0.00956°
Longitude
165.80858°
Altitude
35,793.637 km
Speed
3.074 km/s
True Right ascension
00h 00m 00s
True Declination
0° 00' 34"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
12:21:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,797.282 km
Perigee altitude
35,778.501 km
Semi-major axis
42,166.029 km
Eccentricity
0.00022
Inclination
0.0578°
RAAN
351.7333°
Arg. of periapsis
227.1945°
True anomaly
141.07044°
Mean anomaly
141.0544°
Eccentric anomaly
141.06242°
Mean motion
0.25067 °/min
Orbital period
1,436.16 mins
BSTAR
0
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Other satellites on launch #16 in the year 2023 (2023-02-05 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ELEKTRO-L 4 Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| ELEKTRO-L 4 is likely not visible in the next few days. |
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55506 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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