EKRAN 2 DEB, 11581

Orbit data source: Space-Track

EKRAN 2 DEB, 11581 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

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Iframe URL

https://www.satcat.com/sats-embedded/11581?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

11581, 1977-092H

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

Large (>1 m²)

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Last TLE update: 10 hours ago

TLE from 10 hours ago

0 EKRAN 2 DEB
1 11581U 77092H   26061.73600796  .00000127  00000-0  00000+0 0  9993
2 11581   4.4130 275.4860 0007152 288.4263 248.0898  1.00322393103297

Epoch: 2026-03-02T17:39Z

TLE epoch observation values (Epoch: 2026-03-02T17:39:51.087Z)

Latitude

0.25445°

Longitude

26.49827°

Altitude

35,782.956 km

Speed

3.074 km/s

True Right ascension

06h 07m 56s

True Declination

0° 15' 15"

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

07:13:18

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,803.622 km

Perigee altitude

35,743.328 km

Semi-major axis

42,151.612 km

Eccentricity

0.00072

Inclination

4.413°

RAAN

275.486°

Arg. of periapsis

288.4263°

True anomaly

248.01379°

Mean anomaly

248.0898°

Eccentric anomaly

248.05179°

Mean motion

0.2508 °/min

Orbital period

1,435.43 mins

BSTAR

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

EKRAN 2 DEB, 59986

EKRAN 2 DEB, 59987

SL-12 PLAT, 10367 (Decayed)

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

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

SL-12 DEB, 10368 (Decayed)

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

EKRAN 2 DEB, 29014

EKRAN 2 DEB, 33519

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EKRAN 2 DEB Visibility

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

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11581 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, 11581 on other resources

View EKRAN 2 DEB, 11581 on Heavens-Above

View EKRAN 2 DEB, 11581 on Keep Track

View EKRAN 2 DEB, 11581 on Celestrak

View EKRAN 2 DEB, 11581 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, 11581

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-03-02T17:39:51.087Z)

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

11581 neighbors

Co-orbital & Co-planar RSOs

Check out EKRAN 2 DEB, 11581 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago