Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11791
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: 103.994 minutes
Inclination: 71.0039 deg
SMA: 7325.398 km
Apoapsis: 1043.681 km
Periapsis: 850.844 km
RAAN: 136.0519 deg
Eccentricy: 0.0131622
Argument of periapsis: 332.8308 deg
Mean anomaly: 177.4259 deg
Mean motion: 13.84700816 rev/day
Mean motion (dot): -0.00000016 rev/day2
B* drag term: 0.00002351 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 6:32 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22608U 93016S 25187.27230212 -.00000016 00000-0 23510-4 0 9992
TLE line 2: 2 22608 71.0039 136.0519 0131622 332.8308 177.4259 13.84700816631055
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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