Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11950
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: 1993-016S
Object number (NORAD): 22608
Object ID (CCSDS): 22608
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 103.992 minutes
Inclination: 71.0021 deg
SMA: 7325.342 km
Apoapsis: 1041.334 km
Periapsis: 853.079 km
RAAN: 179.1423 deg
Eccentricy: 0.0128496
Argument of periapsis: 104.3647 deg
Mean anomaly: 4.1161 deg
Mean motion: 13.84716732 rev/day
Mean motion (dot): 0.00000016 rev/day2
B* drag term: 0.000049077 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 7:26 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 11, 2025, 11:19 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22608U 93016S 25345.97160174 .00000016 00000-0 49077-4 0 9999
TLE line 2: 2 22608 71.0021 179.1423 0128496 104.3647 4.1161 13.84716732653024
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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