Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11990
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.2
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: 1992-093DL
Object number (NORAD): 22419
Object ID (CCSDS): 22419
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.155 minutes
Inclination: 71.1779 deg
SMA: 7285.974 km
Apoapsis: 985.122 km
Periapsis: 830.557 km
RAAN: 284.6028 deg
Eccentricy: 0.01060704
Argument of periapsis: 191.8092 deg
Mean anomaly: 168.0534 deg
Mean motion: 13.95954635 rev/day
Mean motion (dot): 0.00000341 rev/day2
B* drag term: 0.00026837383 1/REarth
Two-line elements (TLE)
Creation date: Oct. 23, 2025, 2:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 22, 2025, 11:12 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22419U 92093DL 25295.96732756 .00000341 00000-0 26837-3 0 9996
TLE line 2: 2 22419 71.1779 284.6028 0106070 191.8092 168.0534 13.95954635667989
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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