Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11946
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.3
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: 1992-093KK
Object number (NORAD): 39719
Object ID (CCSDS): 39719
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.138 minutes
Inclination: 71.2967 deg
SMA: 7285.178 km
Apoapsis: 979.119 km
Periapsis: 834.967 km
RAAN: 93.8572 deg
Eccentricy: 0.00989352
Argument of periapsis: 314.1861 deg
Mean anomaly: 66.4255 deg
Mean motion: 13.96183615 rev/day
Mean motion (dot): 0.00000122 rev/day2
B* drag term: 0.00011578556 1/REarth
Two-line elements (TLE)
Creation date: Sept. 6, 2025, 2:09 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 5, 2025, 8:28 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39719U 92093KK 25248.85321807 .00000122 00000-0 11579-3 0 9998
TLE line 2: 2 39719 71.2967 93.8572 0098935 314.1861 66.4255 13.96183615580155
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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