Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12042
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: 102.98 minutes
Inclination: 70.6609 deg
SMA: 7277.736 km
Apoapsis: 999.133 km
Periapsis: 800.069 km
RAAN: 121.7448 deg
Eccentricy: 0.0136762
Argument of periapsis: 155.6345 deg
Mean anomaly: 354.8676 deg
Mean motion: 13.98325643 rev/day
Mean motion (dot): 0.00002962 rev/day2
B* drag term: 0.0019451 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 7:16 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 11, 2025, 7:46 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22326U 92093P 25345.82376580 .00002962 00000-0 19451-2 0 9997
TLE line 2: 2 22326 70.6609 121.7448 0136762 155.6345 354.8676 13.98325643668289
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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