ELEKTRO-L 5, 67756
Orbit data source: Space-Track
ELEKTRO-L 5, 67756 is a Commonwealth of Independent States-origin payload satellite in GEO that was launched on Thu, 12 Feb 2026 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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67756 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Lavochkin
Mission
Operational Civil Weather
Bus & Motor
NAVIGATOR, Unknown motor
Mass
2,120 kg wet, 1,550 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan + 1 Ant, 1.1 m
Radar Cross Section
11.105 m²
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 ELEKTRO-L 5
1 67756U 26028A 26144.11726839 -.00000103 00000-0 00000+0 0 9997
2 67756 0.2989 303.6307 0001431 182.0181 234.3603 1.00271374 1011Epoch: 2026-05-24T02:48Z
TLE epoch observation values (Epoch: 2026-05-24T02:48:51.988Z)
Latitude
0.26493°
Longitude
76.059°
Altitude
35,789.658 km
Speed
3.074 km/s
True Right ascension
23h 59m 59s
True Declination
0° 15' 53"
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
01:27:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,793.814 km
Perigee altitude
35,781.747 km
Semi-major axis
42,165.918 km
Eccentricity
0.00014
Inclination
0.2989°
RAAN
303.6307°
Arg. of periapsis
182.0181°
True anomaly
234.34697°
Mean anomaly
234.3603°
Eccentric anomaly
234.35364°
Mean motion
0.25067 °/min
Orbital period
1,436.16 mins
BSTAR
0
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Other satellites on launch #28 in the year 2026 (2026-02-12 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 5 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 5 is likely not visible in the next few days. |
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67756 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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