Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11884
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: 103.139 minutes
Inclination: 71.2966 deg
SMA: 7285.23 km
Apoapsis: 977.168 km
Periapsis: 837.023 km
RAAN: 212.1585 deg
Eccentricy: 0.0096184
Argument of periapsis: 43.874 deg
Mean anomaly: 129.6371 deg
Mean motion: 13.96168495 rev/day
Mean motion (dot): 0.00000028 rev/day2
B* drag term: 0.000049361 1/REarth
Two-line elements (TLE)
Creation date: July 9, 2025, 2:22 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 8, 2025, 8:20 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39719U 92093KK 25189.84740715 .00000028 00000-0 49361-4 0 9990
TLE line 2: 2 39719 71.2966 212.1585 0096184 43.8740 129.6371 13.96168495571914
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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