Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11906
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: 101.619 minutes
Inclination: 70.9256 deg
SMA: 7213.434 km
Apoapsis: 894.797 km
Periapsis: 775.801 km
RAAN: 319.9794 deg
Eccentricy: 0.00824819
Argument of periapsis: 208.016 deg
Mean anomaly: 214.0552 deg
Mean motion: 14.17064603 rev/day
Mean motion (dot): 0.00001383 rev/day2
B* drag term: 0.00068760551 1/REarth
Two-line elements (TLE)
Creation date: Oct. 18, 2025, 2:17 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 17, 2025, 10:25 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 29098U 93016AM 25290.43467867 .00001383 00000-0 68761-3 0 9996
TLE line 2: 2 29098 70.9256 319.9794 0082482 208.0160 214.0552 14.17064603636390
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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