Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12043
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: 103.681 minutes
Inclination: 70.8028 deg
SMA: 7310.697 km
Apoapsis: 1055.282 km
Periapsis: 809.841 km
RAAN: 151.6592 deg
Eccentricy: 0.01678644
Argument of periapsis: 351.0529 deg
Mean anomaly: 159.3939 deg
Mean motion: 13.88879599 rev/day
Mean motion (dot): 0.00000823 rev/day2
B* drag term: 0.00064207711 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 11:30 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 9:40 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22453U 92093ES 25347.90340753 .00000823 00000-0 64208-3 0 9997
TLE line 2: 2 22453 70.8028 151.6592 0167864 351.0529 159.3939 13.88879599661402
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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