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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https://www.satcat.com/sats-embedded/12996?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

12996, 1977-092J

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 (49 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

Large (>1 m²)

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Last TLE update: 14 hours ago

TLE from 14 hours ago

0 EKRAN 2 DEB
1 12996U 77092J   26182.35527133 -.00000198  00000-0  00000-0 0  9999
2 12996   4.2689 274.6665 0017009 278.1233 136.7817  1.00033010 84651

Epoch: 2026-07-01T08:31Z

TLE epoch observation values (Epoch: 2026-07-01T08:31:35.442Z)

Latitude

3.48368°

Longitude

-77.68395°

Altitude

35,904.869 km

Speed

3.069 km/s

True Right ascension

21h 58m 30s

True Declination

3° 28' 49"

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

10:38:19

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,926.559 km

Perigee altitude

35,782.892 km

Semi-major axis

42,232.862 km

Eccentricity

0.0017

Inclination

4.2689°

RAAN

274.6665°

Arg. of periapsis

278.1233°

True anomaly

136.91496°

Mean anomaly

136.7817°

Eccentric anomaly

136.84835°

Mean motion

0.25007 °/min

Orbital period

1,439.58 mins

BSTAR

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

EKRAN 2, 10365

EKRAN 2 DEB, 59987

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

SL-12 PLAT, 10367 (Decayed)

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

SL-12 DEB, 10368 (Decayed)

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

EKRAN 2 DEB, 33519

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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	2026-07-01 22:58:46.409Z	144.346° SSE	2026-07-02 11:02:46.409Z	139.258° SSE	33.013°	2026-07-02 22:58:46.409Z	145.341° SSE

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12996 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, 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.

EKRAN 2 DEB, 12996

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-07-01T08:31:35.442Z)

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

12996 neighbors

Co-orbital & Co-planar RSOs

Check out EKRAN 2 DEB, 12996 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago