Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11951
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: 1993-016C
Object number (NORAD): 22575
Object ID (CCSDS): 22575
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.853 minutes
Inclination: 71.0057 deg
SMA: 7365.705 km
Apoapsis: 1136.747 km
Periapsis: 838.393 km
RAAN: 300.584 deg
Eccentricy: 0.02025291
Argument of periapsis: 70.0352 deg
Mean anomaly: 45.1391 deg
Mean motion: 13.73350155 rev/day
Mean motion (dot): 0.00000213 rev/day2
B* drag term: 0.00023655469 1/REarth
Two-line elements (TLE)
Creation date: Dec. 13, 2025, 5:47 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 7:09 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22575U 93016C 25347.29836330 .00000213 00000-0 23655-3 0 9995
TLE line 2: 2 22575 71.0057 300.5840 0202529 70.0352 45.1391 13.73350155638698
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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