Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11983
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
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: 1992-076E
Object number (NORAD): 22223
Object ID (CCSDS): 22223
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.645 minutes
Inclination: 71.0375 deg
SMA: 7355.96 km
Apoapsis: 1121.57 km
Periapsis: 834.079 km
RAAN: 123.7761 deg
Eccentricy: 0.01954134
Argument of periapsis: 274.1873 deg
Mean anomaly: 191.162 deg
Mean motion: 13.76080254 rev/day
Mean motion (dot): 0.00000085 rev/day2
B* drag term: 0.0001157757 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 3:16 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 7, 2025, 10:26 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22223U 92076E 25250.93507881 .00000085 00000-0 11578-3 0 9998
TLE line 2: 2 22223 71.0375 123.7761 0195413 274.1873 191.1620 13.76080254646381
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 11’, on board a Zenit-2 space rocket.
The launch took place on Nov. 17, 1992, 7:47 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 11
Agency: N/A
Status: Launch Successful
Launch date: Nov. 17, 1992, 7:47 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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