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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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, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 4 days ago

TLE from 4 days ago

0 ELEKTRON 3 DEB
1 29008U 64038G   26026.15757033  .00004911  00000-0  12913-2 0  9990
2 29008  60.8516 342.8772 2858125 355.5433   2.4211  9.37088335718641

Epoch: 2026-01-26T03:46Z

TLE epoch observation values (Epoch: 2026-01-26T03:46:54.076Z)

Latitude

-0.00002°

Longitude

160.69452°

Altitude

415.153 km

Speed

8.686 km/s

True Right ascension

22h 51m 30s

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

01:17:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

5,840.555 km

Perigee altitude

408.573 km

Semi-major axis

9,502.701 km

Eccentricity

0.28581

Inclination

60.8516°

RAAN

342.8772°

Arg. of periapsis

355.5433°

True anomaly

4.54654°

Mean anomaly

2.4211°

Eccentric anomaly

3.38922°

Mean motion

2.343 °/min

Orbital period

153.65 mins

BSTAR

0.0012913

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

ELEKTRON 4, 830 (Decayed)

SL-3 R/B, 832 (Decayed)

ELEKTRON 3 DEB, 5892 (Decayed)

ELEKTRON 3 DEB, 831

ELEKTRON 3, 829

ELEKTRON 3 DEB, 5893 (Decayed)

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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.
17 mins	2026-01-30 00:08:50.077Z	267.886° W	2026-01-30 00:13:50.077Z	329.883° NNW	31.472°	2026-01-30 00:25:50.077Z	38.75° NE
29 mins	2026-01-30 02:51:50.077Z	322.556° NNW	2026-01-30 02:59:50.077Z	14.346° NNE	28.408°	2026-01-30 03:20:50.077Z	74.813° E
50 mins	2026-01-30 05:31:50.077Z	325.484° NNW	2026-01-30 05:46:50.077Z	45.512° ENE	42.372°	2026-01-30 06:21:50.077Z	129.656° SE
53 mins	2026-01-30 08:11:50.077Z	314.76° NW	2026-01-30 08:30:50.077Z	247.615° W	40.177°	2026-01-30 09:04:50.077Z	178.988° S
21 mins	2026-01-30 11:00:50.077Z	286.803° WNW	2026-01-30 11:09:50.077Z	268.297° W	13.238°	2026-01-30 11:21:50.077Z	247.271° WSW
14 mins	2026-01-30 23:10:50.077Z	247.495° WSW	2026-01-30 23:14:50.077Z	335.186° NNW	39.499°	2026-01-30 23:24:50.077Z	36.679° NE

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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: 4 days ago

TLE from 4 days ago

TLE epoch observation values (Epoch: 2026-01-26T03:46:54.076Z)

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: 4 days ago