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.

Not visible in the next 10 days

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Iframe URL

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 (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

RCS unknown

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Last TLE update: 10 hours ago

TLE from 10 hours ago

0 EKRAN 2 DEB
1 59988U 77092P   26061.73878131  .00000059  00000-0  00000+0 0  9990
2 59988   4.2090 272.9596 0051130  65.5743 128.1635  1.00880694 73974

Epoch: 2026-03-02T17:43Z

TLE epoch observation values (Epoch: 2026-03-02T17:43:50.705Z)

Latitude

-1.04614°

Longitude

40.68172°

Altitude

35,750.688 km

Speed

3.071 km/s

True Right ascension

07h 08m 41s

True Declination

-1° 02' 42"

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

07:19:29

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,832.546 km

Perigee altitude

35,403.096 km

Semi-major axis

41,995.958 km

Eccentricity

0.00511

Inclination

4.209°

RAAN

272.9596°

Arg. of periapsis

65.5743°

True anomaly

128.62235°

Mean anomaly

128.1635°

Eccentric anomaly

128.39311°

Mean motion

0.25219 °/min

Orbital period

1,427.48 mins

BSTAR

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

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

EKRAN 2 DEB, 12996

EKRAN 2 DEB, 33519

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

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

SL-12 R/B(2), 11571

SL-12 PLAT, 10367 (Decayed)

EKRAN 2 DEB, 29014

SL-12 DEB, 10368 (Decayed)

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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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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: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-03-02T17:43:50.705Z)

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

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: 10 hours ago