SL-8 DEB, 1392

Orbit data source: Space-Track

SL-8 DEB, 1392 is space debris in LEO originally from a launch on Mon, 15 Mar 1965 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 URL

https://www.satcat.com/sats-embedded/1392?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

1392, 1965-020AH

Orbit

LEO

Last TLE update

19 hours ago

Origin

Russian Strategic Rocket Forces (CIS)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1965-03-15 (60 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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 19 hours ago

0 SL-8 DEB
1 01392U 65020AH  25221.27093887  .00034698  00000-0  21050-2 0  9994
2 01392  55.8634  93.6694 0192688 105.0748 257.1680 14.96082359 49081

Epoch: 2025-08-09T06:30Z

TLE epoch observation values (Epoch: 2025-08-09T06:30:09.118Z)

Latitude

-0.00003°

Longitude

38.12235°

Altitude

612.398 km

Speed

7.536 km/s

True Right ascension

06h 14m 40s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-35.23219°

Longitude

6.40486°

Altitude

706.48 km

Speed

7.439 km/s

Apparent Right ascension

03h 58m 26s

Apparent Declination

-37° 18' 09"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

15:47:20

Azimuth

319.483° NNW

Elevation

-86.606°

Doppler factor

Orbital elements

Apogee altitude

712.897 km

Perigee altitude

444.792 km

Semi-major axis

6,956.981 km

Eccentricity

0.01927

Inclination

55.8634°

RAAN

93.6694°

Arg. of periapsis

105.0748°

True anomaly

255.02706°

Mean anomaly

257.168°

Eccentric anomaly

256.09633°

Mean motion

3.74035 °/min

Orbital period

96.25 mins

BSTAR

0.002105

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Other satellites on launch #20 in the year 1965 (1965-03-15 UTC)

COSMOS 61, 1267 (Decayed)

SL-8 DEB, 1355 (Decayed)

SL-8 DEB, 1356 (Decayed)

SL-8 DEB, 1370 (Decayed)

SL-8 DEB, 1371 (Decayed)

SL-8 DEB, 1372 (Decayed)

SL-8 DEB, 1373 (Decayed)

SL-8 DEB, 1375 (Decayed)

SL-8 DEB, 1397 (Decayed)

SL-8 DEB, 1398 (Decayed)

SL-8 DEB, 1400 (Decayed)

SL-8 DEB, 1401 (Decayed)

SL-8 DEB, 1402 (Decayed)

SL-8 DEB, 1403 (Decayed)

SL-8 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.
5 mins	2025-08-10 02:17:39.473Z	284.611° WNW	2025-08-10 02:19:39.473Z	245.558° WSW	22.45°	2025-08-10 02:22:39.473Z	180.204° SSW
6 mins	2025-08-10 17:57:39.473Z	232.771° WSW	2025-08-10 18:00:39.473Z	325.949° NNW	43.674°	2025-08-10 18:03:39.473Z	40.744° NE
6 mins	2025-08-11 00:41:39.473Z	326.874° NNW	2025-08-11 00:44:39.473Z	55.416° ENE	36.957°	2025-08-11 00:47:39.473Z	116.96° SE

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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Check out SL-8 DEB, 1392 on other resources

View SL-8 DEB, 1392 on Heavens-Above

View SL-8 DEB, 1392 on Keep Track

View SL-8 DEB, 1392 on Celestrak

View SL-8 DEB, 1392 on Gunter's Space Page

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