ELEKTRO-L 2, 41105
Orbit data source: Space-Track
ELEKTRO-L 2, 41105 is a Commonwealth of Independent States-origin payload satellite in GEO that was launched on Fri, 11 Dec 2015 UTC via a ZENIT-3SLBF 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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41105 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Lavochkin
Mission
Operational Civil Weather
Bus & Motor
NAVIGATOR, Unknown motor
Mass
1,855 kg wet, 1,591 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: 10 hours ago
TLE from 10 hours ago
0 ELEKTRO-L 2
1 41105U 15074A 26087.25662619 -.00000132 00000-0 00000-0 0 9995
2 41105 6.4915 71.5035 0002854 245.3315 306.7306 1.00271696 37693Epoch: 2026-03-28T06:09Z
TLE epoch observation values (Epoch: 2026-03-28T06:09:32.502Z)
Latitude
-1.33521°
Longitude
-14.57991°
Altitude
35,779.154 km
Speed
3.075 km/s
True Right ascension
17h 33m 56s
True Declination
-1° 20' 02"
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
21:39:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,799.704 km
Perigee altitude
35,775.636 km
Semi-major axis
42,165.807 km
Eccentricity
0.00029
Inclination
6.4915°
RAAN
71.5035°
Arg. of periapsis
245.3315°
True anomaly
306.70438°
Mean anomaly
306.7306°
Eccentric anomaly
306.71749°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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Other satellites on launch #74 in the year 2015 (2015-12-11 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 2 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 2 is likely not visible in the next few days. |
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41105 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 descending 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 descending order |
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