Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11338
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: 104.789 minutes
Inclination: 71.0213 deg
SMA: 7362.71 km
Apoapsis: 1130.582 km
Periapsis: 838.567 km
RAAN: 158.3906 deg
Eccentricy: 0.0198307
Argument of periapsis: 178.3053 deg
Mean anomaly: 181.8766 deg
Mean motion: 13.74188313 rev/day
Mean motion (dot): 0.0000008 rev/day2
B* drag term: 0.00011264 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 11:25 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23089U 94023C 25127.47584190 .00000080 00000-0 11264-3 0 9990
TLE line 2: 2 23089 71.0213 158.3906 0198307 178.3053 181.8766 13.74188313555916
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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