EKRAN 2 DEB, 59986

Orbit data source: Space-Track

EKRAN 2 DEB, 59986 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/59986?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59986, 1977-092M

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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago

0 EKRAN 2 DEB
1 59986U 77092M   26171.36267514  .00000068  00000-0  00000+0 0  9996
2 59986   3.7670 270.7834 0041537 120.5644 219.9262  1.00937520 46553

Epoch: 2026-06-20T08:42Z

TLE epoch observation values (Epoch: 2026-06-20T08:42:15.132Z)

Latitude

-1.29614°

Longitude

-148.12437°

Altitude

35,734.825 km

Speed

3.072 km/s

True Right ascension

16h 44m 04s

True Declination

-1° 17' 41"

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

21:40:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,776.433 km

Perigee altitude

35,427.687 km

Semi-major axis

41,980.197 km

Eccentricity

0.00415

Inclination

3.767°

RAAN

270.7834°

Arg. of periapsis

120.5644°

True anomaly

219.62193°

Mean anomaly

219.9262°

Eccentric anomaly

219.77394°

Mean motion

0.25233 °/min

Orbital period

1,426.68 mins

BSTAR

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

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

EKRAN 2 DEB, 33519

EKRAN 2 DEB, 29014

SL-12 PLAT, 10367 (Decayed)

EKRAN 2 DEB, 59987

EKRAN 2, 10365

SL-12 DEB, 10368 (Decayed)

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

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

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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	2026-06-22 10:38:41.481Z	231.648° WSW	2026-06-22 16:18:41.481Z	232.764° WSW	28.715°	2026-06-23 10:38:41.481Z	229.345° WSW

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59986 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, 59986 on other resources

View EKRAN 2 DEB, 59986 on Heavens-Above

View EKRAN 2 DEB, 59986 on Keep Track

View EKRAN 2 DEB, 59986 on Celestrak

View EKRAN 2 DEB, 59986 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, 59986

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-06-20T08:42:15.132Z)

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

59986 neighbors

Co-orbital & Co-planar RSOs

Check out EKRAN 2 DEB, 59986 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago