Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11918
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: 104.646 minutes
Inclination: 71.0373 deg
SMA: 7356.02 km
Apoapsis: 1120.046 km
Periapsis: 835.725 km
RAAN: 252.2112 deg
Eccentricy: 0.0193257
Argument of periapsis: 7.132 deg
Mean anomaly: 104.7368 deg
Mean motion: 13.76063192 rev/day
Mean motion (dot): 0.00000042 rev/day2
B* drag term: 0.000075921 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 6:39 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 2:04 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22223U 92076E 25185.58662308 .00000042 00000-0 75921-4 0 9998
TLE line 2: 2 22223 71.0373 252.2112 0193257 7.1320 104.7368 13.76063192637394
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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