Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11951
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.9
Latest
Satellite identification and parameters
Extended collection of information and parameters for SL-16 DEB.
Object identification
Identified? True
Debris? True
Object name: SL-16 DEB
International designator: 1993-016AM
Object number (NORAD): 29098
Object ID (CCSDS): 29098
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.605 minutes
Inclination: 70.9242 deg
SMA: 7212.816 km
Apoapsis: 891.79 km
Periapsis: 777.572 km
RAAN: 207.9208 deg
Eccentricy: 0.00791771
Argument of periapsis: 127.1721 deg
Mean anomaly: 53.3313 deg
Mean motion: 14.17246718 rev/day
Mean motion (dot): 0.0000167 rev/day2
B* drag term: 0.00082464144 1/REarth
Two-line elements (TLE)
Creation date: Dec. 9, 2025, 5:41 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 9, 2025, 9:30 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 29098U 93016AM 25343.39647583 .00001670 00000-0 82464-3 0 9990
TLE line 2: 2 29098 70.9242 207.9208 0079177 127.1721 53.3313 14.17246718643893
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
Associated space launch
Second generation ELING satellite
SL-16 DEB was lifted into orbit during the mission ‘Zenit-2 | Tselina-2 13’, on board a Zenit-2 space rocket.
The launch took place on March 26, 1993, 2:21 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 13
Agency: N/A
Status: Launch Successful
Launch date: March 26, 1993, 2:21 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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