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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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<iframe src="https://www.satcat.com/sats-embedded/59986?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/59986?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

59986, 1977-092M

Orbit

GEO

Last TLE update

2 months 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 months ago

0 EKRAN 2 DEB
1 59986U 77092M   25063.50428439  .00000002  00000-0  00000-0 0  9995
2 59986   4.9794 277.8818 0041659  99.5170 126.3351  1.00930830 41784

Epoch: 2025-03-04T12:06Z

Definitive object data (Epoch: 2025-03-04T12:06:10.171Z)

Latitude

-3.59899°

Longitude

159.99442°

Altitude

35,707.848 km

Speed

3.074 km/s

True Right ascension

09h 36m 10s

True Declination

-3° 35' 43"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-4.20854°

Longitude

-127.64304°

Altitude

35,769.556 km

Speed

3.069 km/s

Apparent Right ascension

14h 50m 52s

Apparent Declination

-10° 06' 40"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

10:08:17

Azimuth

110.323° ESE

Elevation

7.909°

Doppler factor

1

Orbital elements

Apogee altitude

35,778.803 km

Perigee altitude

35,429.017 km

Semi-major axis

41,982.047 km

Eccentricity

0.0041659

Inclination

4.9794°

RAAN

277.8818°

Arg. of periapsis

99.517°

True anomaly

126.71847°

Mean anomaly

126.3351°

Eccentric anomaly

126.5269°

Mean motion

0.25232 °/min

BSTAR

Unknown

Orbital period

1426.77 mins

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59986 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, 59987

EKRAN 2 DEB, 59988

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.
697 mins	2025-05-10 05:10:15.416Z	107.904° ESE	2025-05-10 11:02:15.416Z	102.874° ESE	13.156°	2025-05-10 16:47:15.416Z	104.709° ESE

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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.

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