Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11398
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: 104.788 minutes
Inclination: 71.0233 deg
SMA: 7362.669 km
Apoapsis: 1129.164 km
Periapsis: 839.904 km
RAAN: 40.0759 deg
Eccentricy: 0.0196437
Argument of periapsis: 91.7242 deg
Mean anomaly: 270.6369 deg
Mean motion: 13.74199745 rev/day
Mean motion (dot): 0.00000049 rev/day2
B* drag term: 0.000083848 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 10:26 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 7:40 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23089U 94023C 25187.81990816 .00000049 00000-0 83848-4 0 9993
TLE line 2: 2 23089 71.0233 40.0759 0196437 91.7242 270.6369 13.74199745564402
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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