Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11821
Days in orbit
Revolutions
≈ 14.6
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.1
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: 1992-093DA
Object number (NORAD): 22409
Object ID (CCSDS): 22409
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 98.591 minutes
Inclination: 71.1326 deg
SMA: 7069.436 km
Apoapsis: 775.796 km
Periapsis: 606.805 km
RAAN: 353.665 deg
Eccentricy: 0.0119522
Argument of periapsis: 281.3797 deg
Mean anomaly: 148.4918 deg
Mean motion: 14.60580998 rev/day
Mean motion (dot): 0.00001135 rev/day2
B* drag term: 0.00022306 1/REarth
Two-line elements (TLE)
Creation date: May 7, 2025, 3:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 6, 2025, 6:37 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22409U 92093DA 25126.77602736 .00001135 00000-0 22306-3 0 9990
TLE line 2: 2 22409 71.1326 353.6650 0119522 281.3797 148.4918 14.60580998689372
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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