Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11941
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.7
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: 1992-093P
Object number (NORAD): 22326
Object ID (CCSDS): 22326
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.006 minutes
Inclination: 70.6632 deg
SMA: 7278.941 km
Apoapsis: 1003.621 km
Periapsis: 797.992 km
RAAN: 328.7451 deg
Eccentricy: 0.01412488
Argument of periapsis: 296.2106 deg
Mean anomaly: 90.098 deg
Mean motion: 13.9797828 rev/day
Mean motion (dot): 0.00001464 rev/day2
B* drag term: 0.00097873238 1/REarth
Two-line elements (TLE)
Creation date: Sept. 3, 2025, 10:15 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 3, 2025, 5:01 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22326U 92093P 25246.20936503 .00001464 00000-0 97873-3 0 9997
TLE line 2: 2 22326 70.6632 328.7451 0141249 296.2106 90.0980 13.97978280654362
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
In-orbit conjunctions
A list of the most updated potential collisions computed for object 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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