Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11882
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.8
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: 1992-093ES
Object number (NORAD): 22453
Object ID (CCSDS): 22453
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.703 minutes
Inclination: 70.8045 deg
SMA: 7311.74 km
Apoapsis: 1056.924 km
Periapsis: 810.287 km
RAAN: 118.0745 deg
Eccentricy: 0.0168658
Argument of periapsis: 220.9664 deg
Mean anomaly: 261.2668 deg
Mean motion: 13.88582321 rev/day
Mean motion (dot): 0.00000427 rev/day2
B* drag term: 0.00035134 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, 4:47 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22453U 92093ES 25187.19960766 .00000427 00000-0 35134-3 0 9998
TLE line 2: 2 22453 70.8045 118.0745 0168658 220.9664 261.2668 13.88582321639090
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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