Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11946
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: 98.572 minutes
Inclination: 71.13 deg
SMA: 7068.551 km
Apoapsis: 771.625 km
Periapsis: 609.207 km
RAAN: 73.1209 deg
Eccentricy: 0.01148873
Argument of periapsis: 73.798 deg
Mean anomaly: 350.3248 deg
Mean motion: 14.60855185 rev/day
Mean motion (dot): 0.00001612 rev/day2
B* drag term: 0.00031168917 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 6:18 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 8, 2025, 2:48 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22409U 92093DA 25251.61709517 .00001612 00000-0 31169-3 0 9994
TLE line 2: 2 22409 71.1300 73.1209 0114887 73.7980 350.3248 14.60855185707604
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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