Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11879
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.2
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: 1992-093BL
Object number (NORAD): 22371
Object ID (CCSDS): 22371
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 103.318 minutes
Inclination: 71.1652 deg
SMA: 7293.655 km
Apoapsis: 995.377 km
Periapsis: 835.663 km
RAAN: 182.2848 deg
Eccentricy: 0.0109488
Argument of periapsis: 67.0201 deg
Mean anomaly: 104.8899 deg
Mean motion: 13.93750176 rev/day
Mean motion (dot): 0.00000118 rev/day2
B* drag term: 0.00011637 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 3:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 3, 2025, 5:35 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22371U 92093BL 25184.73307244 .00000118 00000-0 11637-3 0 9999
TLE line 2: 2 22371 71.1652 182.2848 0109488 67.0201 104.8899 13.93750176650820
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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