Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11855
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: 103.993 minutes
Inclination: 71.0071 deg
SMA: 7325.382 km
Apoapsis: 1044.315 km
Periapsis: 850.179 km
RAAN: 7.6843 deg
Eccentricy: 0.0132509
Argument of periapsis: 241.1346 deg
Mean anomaly: 214.4837 deg
Mean motion: 13.84705339 rev/day
Mean motion (dot): -0.00000002 rev/day2
B* drag term: 0.000035468249 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 6:18 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 8, 2025, 1:17 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22608U 93016S 25251.55371036 -.00000002 00000-0 35468-4 0 9995
TLE line 2: 2 22608 71.0071 7.6843 0132509 241.1346 214.4837 13.84705339639959
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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