Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11883
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.8
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: 1992-093KB
Object number (NORAD): 39711
Object ID (CCSDS): 39711
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.666 minutes
Inclination: 70.8364 deg
SMA: 7262.937 km
Apoapsis: 951.158 km
Periapsis: 818.446 km
RAAN: 271.5949 deg
Eccentricy: 0.0091362
Argument of periapsis: 99.5353 deg
Mean anomaly: 261.6101 deg
Mean motion: 14.02601681 rev/day
Mean motion (dot): 0.00000246 rev/day2
B* drag term: 0.00018295 1/REarth
Two-line elements (TLE)
Creation date: July 1, 2025, 6:11 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 30, 2025, 11:32 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39711U 92093KB 25181.98068370 .00000246 00000-0 18295-3 0 9992
TLE line 2: 2 39711 70.8364 271.5949 0091362 99.5353 261.6101 14.02601681572890
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 12’, on board a Zenit-2 space rocket.
The launch took place on Dec. 25, 1992, 5:56 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 12
Agency: N/A
Status: Launch Successful
Launch date: Dec. 25, 1992, 5:56 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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