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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

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 12996U 77092J   25118.47109081 -.00000184  00000-0  00000-0 0  9993
2 12996   5.3710 280.3849 0012103 271.5402 110.3342  1.00031050 80368

Epoch: 2025-04-28T11:18Z

Definitive object data (Epoch: 2025-04-28T11:18:22.245Z)

Latitude

2.0337°

Longitude

-83.98806°

Altitude

35,871.158 km

Speed

3.071 km/s

True Right ascension

20h 09m 09s

True Declination

2° 01' 54"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

2.07577°

Longitude

-83.45401°

Altitude

35,871.678 km

Speed

3.071 km/s

Apparent Right ascension

20h 21m 12s

Apparent Declination

-3° 51' 50"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

18:53:42

Azimuth

150.076° SSE

Elevation

41.829°

Doppler factor

1

Orbital elements

Apogee altitude

35,906.387 km

Perigee altitude

35,804.157 km

Semi-major axis

42,233.409 km

Eccentricity

0.0012103

Inclination

5.371°

RAAN

280.3849°

Arg. of periapsis

271.5402°

True anomaly

110.46418°

Mean anomaly

110.3342°

Eccentric anomaly

110.3992°

Mean motion

0.25007 °/min

BSTAR

Unknown

Orbital period

1439.61 mins

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12996 neighbors

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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	2025-04-30 11:19:33.287Z	150.087° SSE	2025-04-30 15:54:33.287Z	148.347° SSE	35.408°	2025-05-01 11:19:33.287Z	151.291° SSE

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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