Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11462
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: 104.787 minutes
Inclination: 71.021 deg
SMA: 7362.626 km
Apoapsis: 1130.668 km
Periapsis: 838.313 km
RAAN: 275.1968 deg
Eccentricy: 0.01985396
Argument of periapsis: 0.3132 deg
Mean anomaly: 359.8057 deg
Mean motion: 13.74211852 rev/day
Mean motion (dot): 0.00000103 rev/day2
B* drag term: 0.00013471212 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 6:18 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 8, 2025, 12:15 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23089U 94023C 25251.51096779 .00000103 00000-0 13471-3 0 9992
TLE line 2: 2 23089 71.0210 275.1968 0198540 0.3132 359.8057 13.74211852572958
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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