EKRAN 2 DEB, 59988

Orbit data source: Space-Track

EKRAN 2 DEB, 59988 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/59988?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59988, 1977-092P

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

RCS unknown

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Last TLE update: 1 month ago

TLE from 1 month ago

0 EKRAN 2 DEB
1 59988U 77092P   26134.55788483  .00000130  00000-0  00000-0 0  9992
2 59988   4.0234 271.8693 0044461  85.0066 275.5603  1.00888840 74707

Epoch: 2026-05-14T13:23Z

TLE epoch observation values (Epoch: 2026-05-14T13:23:21.249Z)

Latitude

0.00591°

Longitude

-161.23686°

Altitude

35,597.755 km

Speed

3.082 km/s

True Right ascension

18h 07m 36s

True Declination

0° 00' 21"

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

21:46:02

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,802.269 km

Perigee altitude

35,428.853 km

Semi-major axis

41,993.698 km

Eccentricity

0.00445

Inclination

4.0234°

RAAN

271.8693°

Arg. of periapsis

85.0066°

True anomaly

275.05295°

Mean anomaly

275.5603°

Eccentric anomaly

275.30665°

Mean motion

0.25221 °/min

Orbital period

1,427.37 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, 11581

SL-12 PLAT, 10367 (Decayed)

EKRAN 2 DEB, 12996

SL-12 R/B(2), 11571

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 10:43:58.968Z	133.312° SE	2026-06-22 10:43:58.968Z	133.312° SE	31.105°	2026-06-23 10:43:58.968Z	130.743° SE

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59988 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, 59988 on other resources

View EKRAN 2 DEB, 59988 on Heavens-Above

View EKRAN 2 DEB, 59988 on Keep Track

View EKRAN 2 DEB, 59988 on Celestrak

View EKRAN 2 DEB, 59988 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, 59988

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 month ago

TLE from 1 month ago

TLE epoch observation values (Epoch: 2026-05-14T13:23:21.249Z)

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

59988 neighbors

Co-orbital & Co-planar RSOs

Check out EKRAN 2 DEB, 59988 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 month ago