Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11730
Days in orbit
Revolutions
≈ 14.5
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.1
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: 1993-016F
Object number (NORAD): 22578
Object ID (CCSDS): 22578
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 99.138 minutes
Inclination: 71.0636 deg
SMA: 7095.552 km
Apoapsis: 794.047 km
Periapsis: 640.787 km
RAAN: 330.3625 deg
Eccentricy: 0.0107997
Argument of periapsis: 167.8877 deg
Mean anomaly: 292.7576 deg
Mean motion: 14.52524531 rev/day
Mean motion (dot): 0.00001044 rev/day2
B* drag term: 0.00025002 1/REarth
Two-line elements (TLE)
Creation date: May 7, 2025, 3:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 6, 2025, 8:46 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22578U 93016F 25126.86574003 .00001044 00000-0 25002-3 0 9993
TLE line 2: 2 22578 71.0636 330.3625 0107997 167.8877 292.7576 14.52524531696290
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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