Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11822
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.8
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: 1992-093BA
Object number (NORAD): 22361
Object ID (CCSDS): 22361
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 104.264 minutes
Inclination: 70.7672 deg
SMA: 7338.095 km
Apoapsis: 1095.322 km
Periapsis: 824.598 km
RAAN: 10.602 deg
Eccentricy: 0.0184465
Argument of periapsis: 148.441 deg
Mean anomaly: 239.3213 deg
Mean motion: 13.81108312 rev/day
Mean motion (dot): 0.00000311 rev/day2
B* drag term: 0.00029546 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 10:50 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22361U 92093BA 25127.95145068 .00000311 00000-0 29546-3 0 9996
TLE line 2: 2 22361 70.7672 10.6020 0184465 148.4410 239.3213 13.81108312626773
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 12’, on board a Zenit-2 space rocket.
The launch took place on Dec. 25, 1992, 5:56 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 12
Agency: N/A
Status: Launch Successful
Launch date: Dec. 25, 1992, 5:56 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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