Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11938
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
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: 1992-093CD
Object number (NORAD): 22388
Object ID (CCSDS): 22388
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.617 minutes
Inclination: 70.9631 deg
SMA: 7213.385 km
Apoapsis: 907.035 km
Periapsis: 763.465 km
RAAN: 85.6113 deg
Eccentricy: 0.00995162
Argument of periapsis: 334.878 deg
Mean anomaly: 94.181 deg
Mean motion: 14.17079142 rev/day
Mean motion (dot): 0.00001954 rev/day2
B* drag term: 0.00094718692 1/REarth
Two-line elements (TLE)
Creation date: Aug. 31, 2025, 2:26 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 30, 2025, 4:07 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22388U 92093CD 25242.67189497 .00001954 00000-0 94719-3 0 9994
TLE line 2: 2 22388 70.9631 85.6113 0099516 334.8780 94.1810 14.17079142671236
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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