ELEKTRON 3 DEB, 29008

Orbit data source: Space-Track

ELEKTRON 3 DEB, 29008 is space debris 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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Iframe URL

https://www.satcat.com/sats-embedded/29008?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29008, 1964-038G

Orbit

Active

Country

CIS

Related business

Energia (RU)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1964-07-10 (62 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.050 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 ELEKTRON 3 DEB
1 29008U 64038G   26298.53406060  .00001062  00000-0  25322-3 0  9997
2 29008  60.8304 313.7297 2867691  70.0809 318.4141  9.38088763744185

Epoch: 2026-10-25T12:49Z

TLE epoch observation values (Epoch: 2026-10-25T12:49:02.835Z)

Latitude

0.00002°

Longitude

87.54337°

Altitude

1,559.628 km

Speed

7.648 km/s

True Right ascension

20h 54m 55s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

18:47:29

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

5,840.951 km

Perigee altitude

394.664 km

Semi-major axis

9,495.944 km

Eccentricity

0.28677

Inclination

60.8304°

RAAN

313.7297°

Arg. of periapsis

70.0809°

True anomaly

290.01432°

Mean anomaly

318.4141°

Eccentric anomaly

304.94602°

Mean motion

2.3455 °/min

Orbital period

153.49 mins

BSTAR

0.00025322

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Other satellites on launch #38 in the year 1964 (1964-07-10 UTC)

SL-3 R/B, 832 (Decayed)

ELEKTRON 3 DEB, 5893 (Decayed)

ELEKTRON 3 DEB, 5892 (Decayed)

ELEKTRON 4, 830 (Decayed)

ELEKTRON 3 DEB, 831

ELEKTRON 3, 829

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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	2026-10-27 03:19:34.422Z	222.187° SW	2026-10-27 03:24:34.422Z	354.786° N	64.265°	2026-10-27 03:26:34.422Z	31.35° NE
16 mins	2026-10-27 11:21:34.422Z	325.177° NNW	2026-10-27 11:25:34.422Z	118.451° SE	79.435°	2026-10-27 11:37:34.422Z	143.414° SSE
11 mins	2026-10-27 14:01:34.422Z	263.12° W	2026-10-27 14:05:34.422Z	237.322° WSW	16.283°	2026-10-27 14:12:34.422Z	209.017° SW

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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

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out ELEKTRON 3 DEB, 29008 on other resources

View ELEKTRON 3 DEB, 29008 on Heavens-Above

View ELEKTRON 3 DEB, 29008 on Keep Track

View ELEKTRON 3 DEB, 29008 on Celestrak

View ELEKTRON 3 DEB, 29008 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

ELEKTRON 3 DEB, 29008

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-10-25T12:49:02.835Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #38 in the year 1964 (1964-07-10 UTC)

ELEKTRON 3 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out ELEKTRON 3 DEB, 29008 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago