ELEKTRON 3 DEB, 831
Orbit data source: Space-Track
ELEKTRON 3 DEB, 831 is space debris in LEO originally from a launch on Fri, 10 Jul 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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831 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: 23 hours ago
TLE from 23 hours ago
0 ELEKTRON 3 DEB
1 00831U 64038C 26300.14815230 .00010408 00000-0 85425-3 0 9998
2 00831 60.6615 205.5216 1228376 96.1560 278.0431 12.86798605382892Epoch: 2026-10-27T03:33Z
TLE epoch observation values (Epoch: 2026-10-27T03:33:20.358Z)
Latitude
-0.00004°
Longitude
116.6713°
Altitude
1,299.19 km
Speed
7.215 km/s
True Right ascension
13h 42m 05s
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
21:30:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,258.256 km
Perigee altitude
368.626 km
Semi-major axis
7,691.578 km
Eccentricity
0.12284
Inclination
60.6615°
RAAN
205.5216°
Arg. of periapsis
96.156°
True anomaly
263.94367°
Mean anomaly
278.0431°
Eccentric anomaly
271.00611°
Mean motion
3.21751 °/min
Orbital period
111.89 mins
BSTAR
0.00085425
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Other satellites on launch #38 in the year 1964 (1964-07-10 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 3 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-28 04:20:10.937Z | 316.06° NNW | 2026-10-28 04:22:10.937Z | 287.889° WNW | 62.809° | 2026-10-28 04:27:10.937Z | 148.863° SSE |
| 7 mins | 2026-10-28 18:51:10.937Z | 177.456° S | 2026-10-28 18:55:10.937Z | 114.448° SE | 31.169° | 2026-10-28 18:58:10.937Z | 64.006° ENE |
| 5 mins | 2026-10-28 20:48:10.937Z | 272.497° WNW | 2026-10-28 20:50:10.937Z | 310.284° NW | 25.351° | 2026-10-28 20:53:10.937Z | 9.398° NNE |
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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