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EKRAN 2 DEB, 12996

Orbit data source: Space-Track

EKRAN 2 DEB, 12996 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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<iframe src="https://www.satcat.com/sats-embedded/12996?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/12996?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

12996, 1977-092J

Orbit

GEO

Last TLE update

19 hours 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 19 hours ago

0 EKRAN 2 DEB
1 12996U 77092J   25129.27612979 -.00000125  00000-0  00000-0 0  9993
2 12996   5.3429 280.2437 0012747 267.4629  45.6054  1.00028784 80467

Epoch: 2025-05-09T06:37Z

Definitive object data (Epoch: 2025-05-09T06:37:37.613Z)

Latitude

-3.90418°

Longitude

-93.21127°

Altitude

35,817.083 km

Speed

3.075 km/s

True Right ascension

15h 34m 07s

True Declination

-3° 54' 01"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-4.48795°

Longitude

-169.979°

Altitude

35,808.915 km

Speed

3.076 km/s

Apparent Right ascension

10h 32m 41s

Apparent Declination

-11° 11' 15"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

09:43:51

Azimuth

164.811° S

Elevation

37.655°

Doppler factor

1

Orbital elements

Apogee altitude

35,909.746 km

Perigee altitude

35,802.074 km

Semi-major axis

42,234.047 km

Eccentricity

0.0012747

Inclination

5.3429°

RAAN

280.2437°

Arg. of periapsis

267.4629°

True anomaly

45.70989°

Mean anomaly

45.6054°

Eccentric anomaly

45.65763°

Mean motion

0.25006 °/min

BSTAR

Unknown

Orbital period

1439.64 mins

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12996 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, 29014

EKRAN 2 DEB, 33519

EKRAN 2 DEB, 59986

EKRAN 2 DEB, 59987

EKRAN 2 DEB, 59988

EKRAN 2 DEB Visibility forecast

Observer location: undefined°, undefined°

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	2025-05-10 01:31:53.644Z	164.816° S	2025-05-10 15:49:53.644Z	162.003° S	36.813°	2025-05-11 01:31:53.644Z	166.025° S

Authenticating...

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Check out EKRAN 2 DEB, 12996 on other resources

View EKRAN 2 DEB, 12996 on Heavens-Above

View EKRAN 2 DEB, 12996 on Keep Track

View EKRAN 2 DEB, 12996 on Celestrak

View EKRAN 2 DEB, 12996 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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