Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11558
Days in orbit
Revolutions
≈ 13.7
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: 1994-023C
Object number (NORAD): 23089
Object ID (CCSDS): 23089
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.784 minutes
Inclination: 71.0238 deg
SMA: 7362.479 km
Apoapsis: 1131.47 km
Periapsis: 837.217 km
RAAN: 86.647 deg
Eccentricy: 0.0199833
Argument of periapsis: 224.5641 deg
Mean anomaly: 133.9244 deg
Mean motion: 13.7425301 rev/day
Mean motion (dot): 0.00000138 rev/day2
B* drag term: 0.00016668349 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 3:07 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 3:57 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23089U 94023C 25347.66465928 .00000138 00000-0 16668-3 0 9999
TLE line 2: 2 23089 71.0238 86.6470 0199833 224.5641 133.9244 13.74253010586161
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 15’, on board a Zenit-2 space rocket.
The launch took place on April 23, 1994, 8:01 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 15
Agency: N/A
Status: Launch Successful
Launch date: April 23, 1994, 8:01 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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