Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11920
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: 1992-076C
Object number (NORAD): 22221
Object ID (CCSDS): 22221
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.53 minutes
Inclination: 71.0423 deg
SMA: 7350.564 km
Apoapsis: 1108.481 km
Periapsis: 836.377 km
RAAN: 193.0405 deg
Eccentricy: 0.0185091
Argument of periapsis: 274.7432 deg
Mean anomaly: 203.9931 deg
Mean motion: 13.77595642 rev/day
Mean motion (dot): 0.00000085 rev/day2
B* drag term: 0.00011431 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 11:03 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22221U 92076C 25187.46068082 .00000085 00000-0 11431-3 0 9996
TLE line 2: 2 22221 71.0423 193.0405 0185091 274.7432 203.9931 13.77595642639625
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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