ELEKTRON 1 DEB, 750
Orbit data source: Space-Track
ELEKTRON 1 DEB, 750 is space debris in LEO originally from a launch on Thu, 30 Jan 1964 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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750 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
OKB-1
Mission
Spacecraft
Bus & Motor
ADAPTER, Unknown motor
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 ELEKTRON 1 DEB
1 750U 64006C 26163.85109030 .00020706 00000-0 19058-2 0 9992
2 750 60.7469 353.6013 1385002 62.4789 311.0011 12.51481754846117Epoch: 2026-06-12T20:25Z
TLE epoch observation values (Epoch: 2026-06-12T20:25:34.201Z)
Latitude
-0.00008°
Longitude
146.03414°
Altitude
845.608 km
Speed
7.716 km/s
True Right ascension
23h 34m 24s
True Declination
0° 00' 00"
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
13:37:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,542.723 km
Perigee altitude
372.252 km
Semi-major axis
7,835.625 km
Eccentricity
0.1385
Inclination
60.7469°
RAAN
353.6013°
Arg. of periapsis
62.4789°
True anomaly
297.62181°
Mean anomaly
311.0011°
Eccentric anomaly
304.45797°
Mean motion
3.1292 °/min
Orbital period
115.05 mins
BSTAR
0.0019058
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Other satellites on launch #6 in the year 1964 (1964-01-30 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.ELEKTRON 1 DEB Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-13 21:49:52.935Z | 0.028° NNE | 2026-06-13 21:52:52.935Z | 56.522° ENE | 26.903° | 2026-06-13 21:57:52.935Z | 105.87° ESE |
| 11 mins | 2026-06-13 23:47:52.935Z | 297.428° NW | 2026-06-13 23:51:52.935Z | 224.333° SW | 35.121° | 2026-06-13 23:58:52.935Z | 168.018° S |
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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