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EKRAN 2 DEB, 59987

Orbit data source: Space-Track

EKRAN 2 DEB, 59987 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

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/59987?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/59987?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

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ISO8601 Format

Identifier

59987, 1977-092N

Orbit

GEO

Last TLE update

2 days ago

Origin

Main Directorate of Ministry of Foreign Affairs (CIS)

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

Radar Cross Section

RCS unknown

Expand to show TLE details & history

TLE from 2 days ago

0 EKRAN 2 DEB
1 59987U 77092N   25185.86827361 -.00000315  00000-0  00000-0 0  9995
2 59987   5.0192 278.6474 0014904 213.9106 232.5689  1.00309755 59633

Epoch: 2025-07-04T20:50Z

TLE epoch observation values (Epoch: 2025-07-04T20:50:18.839Z)

Latitude

5.01563°

Longitude

129.27892°

Altitude

35,813.055 km

Speed

3.072 km/s

True Right ascension

00h 19m 53s

True Declination

5° 00' 38"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-0.08517°

Longitude

-135.83091°

Altitude

35,722.665 km

Speed

3.079 km/s

Apparent Right ascension

06h 19m 05s

Apparent Declination

-5° 14' 09"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

15:00:25

Azimuth

294.352° NW

Elevation

-33.566°

Doppler factor

1

Orbital elements

Apogee altitude

35,839.841 km

Perigee altitude

35,714.185 km

Semi-major axis

42,155.15 km

Eccentricity

0.00149

Inclination

5.0192°

RAAN

278.6474°

Arg. of periapsis

213.9106°

True anomaly

Unknown

Mean anomaly

232.5689°

Eccentric anomaly

Unknown

Mean motion

0.25077 °/min

Orbital period

1,435.61 mins

BSTAR

0

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59987 neighbors

Authenticating...

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

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

SL-12 PLAT, 10367 (Decayed)

SL-12 DEB, 10368 (Decayed)

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

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

SL-12 R/B(2), 11571

EKRAN 2 DEB, 11581

EKRAN 2 DEB, 12996

EKRAN 2 DEB, 29014

EKRAN 2 DEB, 33519

EKRAN 2 DEB, 59986

EKRAN 2 DEB, 59988

EKRAN 2 DEB Visibility

Observer location: undefined°, undefined°

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

Authenticating...

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Check out EKRAN 2 DEB, 59987 on other resources

View EKRAN 2 DEB, 59987 on Heavens-Above

View EKRAN 2 DEB, 59987 on Keep Track

View EKRAN 2 DEB, 59987 on Celestrak

View EKRAN 2 DEB, 59987 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

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