Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12042
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.9
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: 1992-093AD
Object number (NORAD): 22340
Object ID (CCSDS): 22340
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 103.261 minutes
Inclination: 70.874 deg
SMA: 7290.958 km
Apoapsis: 988.257 km
Periapsis: 837.389 km
RAAN: 140.7456 deg
Eccentricy: 0.01034625
Argument of periapsis: 277.2939 deg
Mean anomaly: 258.3906 deg
Mean motion: 13.94523592 rev/day
Mean motion (dot): 0.00000089 rev/day2
B* drag term: 0.000097194203 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 4:30 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22340U 92093AD 25346.18792374 .00000089 00000-0 97194-4 0 9996
TLE line 2: 2 22340 70.8740 140.7456 0103462 277.2939 258.3906 13.94523592676545
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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