Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12041
Days in orbit
Revolutions
≈ 14.6
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.1
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: 1992-093DA
Object number (NORAD): 22409
Object ID (CCSDS): 22409
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 98.546 minutes
Inclination: 71.1312 deg
SMA: 7067.275 km
Apoapsis: 772.947 km
Periapsis: 605.333 km
RAAN: 220.6578 deg
Eccentricy: 0.01185848
Argument of periapsis: 276.7663 deg
Mean anomaly: 209.3621 deg
Mean motion: 14.61250919 rev/day
Mean motion (dot): 0.00001906 rev/day2
B* drag term: 0.00036138428 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 2:41 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22409U 92093DA 25346.11247238 .00001906 00000-0 36138-3 0 9998
TLE line 2: 2 22409 71.1312 220.6578 0118585 276.7663 209.3621 14.61250919721404
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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