Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11729
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: 1993-016AD
Object number (NORAD): 22619
Object ID (CCSDS): 22619
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 104.816 minutes
Inclination: 71.0002 deg
SMA: 7363.973 km
Apoapsis: 1122.804 km
Periapsis: 848.873 km
RAAN: 320.1185 deg
Eccentricy: 0.0185994
Argument of periapsis: 1.8648 deg
Mean anomaly: 9.9197 deg
Mean motion: 13.73834607 rev/day
Mean motion (dot): 0.00000027 rev/day2
B* drag term: 0.000065522 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 8:10 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22619U 93016AD 25125.84096194 .00000027 00000-0 65522-4 0 9998
TLE line 2: 2 22619 71.0002 320.1185 0185994 1.8648 9.9197 13.73834607609153
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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