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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.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/29014?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/29014?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29014, 1977-092K

Orbit

GEO

Last TLE update

2 days ago

Origin

Main Directorate of Ministry of Foreign Affairs (CIS)

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

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 2 days ago

0 EKRAN 2 DEB
1 29014U 77092K   25186.13410010 -.00000098  00000-0  00000-0 0  9991
2 29014   5.0258 278.9245 0018784 335.5113  64.9665  1.00152820 43804

Epoch: 2025-07-05T03:13Z

TLE epoch observation values (Epoch: 2025-07-05T03:13:06.248Z)

Latitude

3.26233°

Longitude

-12.16965°

Altitude

35,785.373 km

Speed

3.076 km/s

True Right ascension

21h 17m 55s

True Declination

3° 15' 33"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

3.31785°

Longitude

-11.26293°

Altitude

35,786.432 km

Speed

3.076 km/s

Apparent Right ascension

21h 47m 58s

Apparent Declination

-2° 11' 51"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

15:13:11

Azimuth

86.089° E

Elevation

-8.076°

Doppler factor

1

Orbital elements

Apogee altitude

35,900.303 km

Perigee altitude

35,741.769 km

Semi-major axis

42,199.173 km

Eccentricity

0.00188

Inclination

5.0258°

RAAN

278.9245°

Arg. of periapsis

335.5113°

True anomaly

Unknown

Mean anomaly

64.9665°

Eccentric anomaly

Unknown

Mean motion

0.25037 °/min

Orbital period

1,437.86 mins

BSTAR

0

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29014 neighbors

Authenticating...

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

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

SL-12 PLAT, 10367 (Decayed)

SL-12 DEB, 10368 (Decayed)

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

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

SL-12 R/B(2), 11571

EKRAN 2 DEB, 11581

EKRAN 2 DEB, 12996

EKRAN 2 DEB, 33519

EKRAN 2 DEB, 59986

EKRAN 2 DEB, 59987

EKRAN 2 DEB, 59988

EKRAN 2 DEB Visibility

Observer location: undefined°, undefined°

EKRAN 2 DEB is likely not visible in the next few days

Authenticating...

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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.

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