SL-16 DEB, 29100

Orbit data source: Space-Track

SL-16 DEB, 29100 is space debris in LEO originally from a launch on Fri, 26 Mar 1993 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/29100?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29100, 1993-016AP

Orbit

LEO

Last TLE update

3 days ago

Origin

Russian Strategic Rocket Forces (CIS)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1993-03-26 (32 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

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 3 days ago

0 SL-16 DEB
1 29100U 93016AP  25126.63544759  .00001182  00000-0  66202-3 0  9991
2 29100  70.7238 214.0303 0073275 311.6738  47.8123 14.11515980174032

Epoch: 2025-05-06T15:15Z

Definitive object data (Epoch: 2025-05-06T15:15:02.671Z)

Latitude

-0.00005°

Longitude

120.53734°

Altitude

821.187 km

Speed

7.461 km/s

True Right ascension

14h 16m 07s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude

-40.18353°

Longitude

-47.86939°

Altitude

863.98 km

Speed

7.422 km/s

Apparent Right ascension

02h 24m 16s

Apparent Declination

-40° 19' 41"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

13:40:58

Azimuth

263.666° W

Elevation

-81.72°

Doppler factor

Orbital elements

Apogee altitude

905.124 km

Perigee altitude

799.164 km

Semi-major axis

7,230.281 km

Eccentricity

0.0073275

Inclination

70.7238°

RAAN

214.0303°

Arg. of periapsis

311.6738°

True anomaly

48.43829°

Mean anomaly

47.8123°

Eccentric anomaly

48.12491°

Mean motion

3.53029 °/min

BSTAR

0.00066202

Orbital period

101.97 mins

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Other satellites on launch #16 in the year 1993 (1993-03-26 UTC)

SL-16 DEB, 22661 (Decayed)

SL-16 DEB, 23304 (Decayed)

SL-16 DEB, 26968

SL-16 DEB *, 29096 (Decayed)

SL-16 DEB, 29097

SL-16 DEB, 29098

SL-16 DEB, 29099 (Decayed)

SL-16 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.
10 mins	2025-05-09 06:17:17.709Z	180.047° SSW	2025-05-09 06:22:17.709Z	106.366° ESE	37.6°	2025-05-09 06:27:17.709Z	35.295° NE
7 mins	2025-05-09 08:04:17.709Z	269.004° W	2025-05-09 08:07:17.709Z	312.422° NW	22.506°	2025-05-09 08:11:17.709Z	358.278° N
8 mins	2025-05-09 15:14:17.709Z	6.579° NNE	2025-05-09 15:18:17.709Z	57.765° ENE	23.587°	2025-05-09 15:22:17.709Z	105.311° ESE
10 mins	2025-05-09 16:58:17.709Z	322.206° NNW	2025-05-09 17:02:17.709Z	267.581° W	37.573°	2025-05-09 17:08:17.709Z	178.747° S

Authenticating...

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Check out SL-16 DEB, 29100 on other resources

View SL-16 DEB, 29100 on Heavens-Above

View SL-16 DEB, 29100 on Keep Track

View SL-16 DEB, 29100 on Celestrak

View SL-16 DEB, 29100 on Gunter's Space Page

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