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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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<iframe src="https://www.satcat.com/sats-embedded/59988?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/59988?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59988, 1977-092P

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 59988U 77092P   25187.35720149 -.00000041  00000-0  00000-0 0  9994
2 59988   4.8235 276.5162 0041118  78.9637 294.9693  1.00884031 71563

Epoch: 2025-07-06T08:34Z

TLE epoch observation values (Epoch: 2025-07-06T08:34:22.208Z)

Latitude

1.10396°

Longitude

-123.20398°

Altitude

35,542.936 km

Speed

3.086 km/s

True Right ascension

19h 19m 52s

True Declination

1° 06' 10"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

1.58763°

Longitude

-117.19869°

Altitude

35,526.864 km

Speed

3.087 km/s

Apparent Right ascension

19h 36m 45s

Apparent Declination

-4° 28' 51"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

20:38:35

Azimuth

201.445° SSW

Elevation

43.381°

Doppler factor

1

Orbital elements

Apogee altitude

35,789.567 km

Perigee altitude

35,444.217 km

Semi-major axis

41,995.029 km

Eccentricity

0.00411

Inclination

4.8235°

RAAN

276.5162°

Arg. of periapsis

78.9637°

True anomaly

Unknown

Mean anomaly

294.9693°

Eccentric anomaly

Unknown

Mean motion

0.2522 °/min

Orbital period

1,427.43 mins

BSTAR

0

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59988 neighbors

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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, 59987

EKRAN 2 DEB Visibility forecast

Observer location: undefined°, undefined°

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	2025-07-08 08:32:51.381Z	201.437° SSW	2025-07-08 13:27:51.381Z	201.251° SSW	36.248°	2025-07-09 08:32:51.381Z	198.206° SSW

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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.

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