Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11951
Days in orbit
Revolutions
≈ 13.9
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: 1993-016Z
Object number (NORAD): 22615
Object ID (CCSDS): 22615
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.296 minutes
Inclination: 71.0024 deg
SMA: 7292.59 km
Apoapsis: 1008.961 km
Periapsis: 819.949 km
RAAN: 91.4462 deg
Eccentricy: 0.01295919
Argument of periapsis: 35.44 deg
Mean anomaly: 22.7098 deg
Mean motion: 13.9405552 rev/day
Mean motion (dot): 0.00001034 rev/day2
B* drag term: 0.00076011219 1/REarth
Two-line elements (TLE)
Creation date: Dec. 11, 2025, 7:14 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 11, 2025, 9:06 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22615U 93016Z 25345.37973763 .00001034 00000-0 76011-3 0 9995
TLE line 2: 2 22615 71.0024 91.4462 0129592 35.4400 22.7098 13.94055520655392
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 13’, on board a Zenit-2 space rocket.
The launch took place on March 26, 1993, 2:21 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 13
Agency: N/A
Status: Launch Successful
Launch date: March 26, 1993, 2:21 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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