Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12044
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: 103.152 minutes
Inclination: 71.1773 deg
SMA: 7285.835 km
Apoapsis: 983.141 km
Periapsis: 832.26 km
RAAN: 175.7913 deg
Eccentricy: 0.01035445
Argument of periapsis: 109.7415 deg
Mean anomaly: 251.4902 deg
Mean motion: 13.95994598 rev/day
Mean motion (dot): 0.00000271 rev/day2
B* drag term: 0.00021924993 1/REarth
Two-line elements (TLE)
Creation date: Dec. 16, 2025, 2:19 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 15, 2025, 10:11 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22419U 92093DL 25349.92458174 .00000271 00000-0 21925-3 0 9996
TLE line 2: 2 22419 71.1773 175.7913 0103544 109.7415 251.4902 13.95994598675512
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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