Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11825
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.3
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: 1992-093AM
Object number (NORAD): 22348
Object ID (CCSDS): 22348
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.21 minutes
Inclination: 71.2591 deg
SMA: 7241.406 km
Apoapsis: 939.48 km
Periapsis: 787.062 km
RAAN: 314.7972 deg
Eccentricy: 0.0105241
Argument of periapsis: 280.6623 deg
Mean anomaly: 243.5403 deg
Mean motion: 14.08861839 rev/day
Mean motion (dot): 0.00000472 rev/day2
B* drag term: 0.00028456 1/REarth
Two-line elements (TLE)
Creation date: May 11, 2025, 2:40 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 10, 2025, 9:52 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22348U 92093AM 25130.91179958 .00000472 00000-0 28456-3 0 9993
TLE line 2: 2 22348 71.2591 314.7972 0105241 280.6623 243.5403 14.08861839656713
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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