Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11951
Days in orbit
Revolutions
≈ 13.8
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: 1993-016N
Object number (NORAD): 22604
Object ID (CCSDS): 22604
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 104.614 minutes
Inclination: 70.9911 deg
SMA: 7354.504 km
Apoapsis: 1101.613 km
Periapsis: 851.125 km
RAAN: 133.0142 deg
Eccentricy: 0.0170296
Argument of periapsis: 343.8857 deg
Mean anomaly: 196.0953 deg
Mean motion: 13.76488864 rev/day
Mean motion (dot): 0.00000016 rev/day2
B* drag term: 0.000054633159 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 4:49 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22604U 93016N 25346.20118166 .00000016 00000-0 54633-4 0 9990
TLE line 2: 2 22604 70.9911 133.0142 0170296 343.8857 196.0953 13.76488864643292
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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