SL-16 DEB, 29098

Orbit data source: Space-Track

SL-16 DEB, 29098 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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https://www.satcat.com/sats-embedded/29098?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29098, 1993-016AM

Orbit

LEO

Last TLE update

18 hours 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 18 hours ago

0 SL-16 DEB
1 29098U 93016AM  25199.22342684  .00001457  00000-0  72723-3 0  9995
2 29098  70.9238 152.8811 0082883 342.8221  80.3579 14.16765557196438

Epoch: 2025-07-18T05:21Z

TLE epoch observation values (Epoch: 2025-07-18T05:21:44.078Z)

Latitude

58.35372°

Longitude

170.0962°

Altitude

836.082 km

Speed

7.446 km/s

True Right ascension

12h 27m 13s

True Declination

58° 12' 06"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-59.98936°

Longitude

98.03015°

Altitude

818.484 km

Speed

7.464 km/s

Apparent Right ascension

03h 04m 32s

Apparent Declination

-64° 35' 51"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:11:22

Azimuth

210.849° SW

Elevation

-54.997°

Doppler factor

Orbital elements

Apogee altitude

894.021 km

Perigee altitude

774.464 km

Semi-major axis

7,212.38 km

Eccentricity

0.00829

Inclination

70.9238°

RAAN

152.8811°

Arg. of periapsis

342.8221°

True anomaly

81.29584°

Mean anomaly

80.3579°

Eccentric anomaly

80.82671°

Mean motion

3.54344 °/min

Orbital period

101.6 mins

BSTAR

0.00072723

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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, 29099 (Decayed)

SL-16 DEB, 29100

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.
6 mins	2025-07-18 23:53:46.703Z	274.03° WNW	2025-07-18 23:56:46.703Z	310.599° NW	16.691°	2025-07-18 23:59:46.703Z	346.024° N
8 mins	2025-07-19 07:02:46.703Z	8.288° NNE	2025-07-19 07:05:46.703Z	51.962° ENE	27.574°	2025-07-19 07:10:46.703Z	116.814° SE
9 mins	2025-07-19 08:45:46.703Z	316.299° NNW	2025-07-19 08:49:46.703Z	261.443° W	32.26°	2025-07-19 08:54:46.703Z	190.84° SSW
9 mins	2025-07-19 21:51:46.703Z	185.775° SSW	2025-07-19 21:55:46.703Z	90.163° ESE	41.642°	2025-07-19 22:00:46.703Z	29.551° NE

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-16 DEB, 29098 on other resources

View SL-16 DEB, 29098 on Heavens-Above

View SL-16 DEB, 29098 on Keep Track

View SL-16 DEB, 29098 on Celestrak

View SL-16 DEB, 29098 on Gunter's Space Page

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