EKRAN 2 DEB, 29014

Orbit data source: Space-Track

EKRAN 2 DEB, 29014 is space debris in GEO originally from a launch on Tue, 20 Sep 1977 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/29014?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29014, 1977-092K

Orbit

GEO

Country

CIS

Related business

Main Directorate of Ministry of Foreign Affairs (RU)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1977-09-20 (48 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 1.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

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Last TLE update: 11 hours ago

TLE from 11 hours ago

0 EKRAN 2 DEB
1 29014U 77092K   26061.60661857  .00000093  00000-0  00000+0 0  9996
2 29014   4.4076 275.7077 0020280 346.9614 336.9560  1.00118937 46203

Epoch: 2026-03-02T14:33Z

TLE epoch observation values (Epoch: 2026-03-02T14:33:31.844Z)

Latitude

-2.57532°

Longitude

-139.11833°

Altitude

35,751.052 km

Speed

3.079 km/s

True Right ascension

15h 58m 38s

True Declination

-2° 34' 22"

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

05:20:58

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,916.158 km

Perigee altitude

35,744.959 km

Semi-major axis

42,208.695 km

Eccentricity

0.00203

Inclination

4.4076°

RAAN

275.7077°

Arg. of periapsis

346.9614°

True anomaly

336.86482°

Mean anomaly

336.956°

Eccentric anomaly

336.91043°

Mean motion

0.25029 °/min

Orbital period

1,438.34 mins

BSTAR

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Other satellites on launch #92 in the year 1977 (1977-09-20 UTC)

SL-12 R/B(AUX MOTOR), 10408 (Decayed)

SL-12 R/B(AUX MOTOR), 10484 (Decayed)

SL-12 R/B(1), 10366 (Decayed)

EKRAN 2 DEB, 33519

SL-12 PLAT, 10367 (Decayed)

SL-12 DEB, 10368 (Decayed)

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EKRAN 2 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.
1440 mins	2026-03-03 01:38:02.143Z	228.961° WSW	2026-03-03 22:58:02.143Z	230.333° WSW	30.299°	2026-03-04 01:38:02.143Z	229.547° WSW

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29014 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

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

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Check out EKRAN 2 DEB, 29014 on other resources

View EKRAN 2 DEB, 29014 on Heavens-Above

View EKRAN 2 DEB, 29014 on Keep Track

View EKRAN 2 DEB, 29014 on Celestrak

View EKRAN 2 DEB, 29014 on Gunter's Space Page

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

EKRAN 2 DEB, 29014

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-03-02T14:33:31.844Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #92 in the year 1977 (1977-09-20 UTC)

EKRAN 2 DEB Visibility forecast

29014 neighbors

Co-orbital & Co-planar RSOs

Check out EKRAN 2 DEB, 29014 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago