Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11936
Days in orbit
Revolutions
≈ 14.6
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.8
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: 1992-093EU
Object number (NORAD): 22455
Object ID (CCSDS): 22455
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.663 minutes
Inclination: 70.8448 deg
SMA: 7072.902 km
Apoapsis: 743.838 km
Periapsis: 645.696 km
RAAN: 250.571 deg
Eccentricy: 0.00693792
Argument of periapsis: 44.5288 deg
Mean anomaly: 22.249 deg
Mean motion: 14.59507449 rev/day
Mean motion (dot): 0.00024633 rev/day2
B* drag term: 0.0050073051 1/REarth
Two-line elements (TLE)
Creation date: Aug. 30, 2025, 3:38 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 29, 2025, 8:43 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22455U 92093EU 25241.86358906 .00024633 00000-0 50073-2 0 9995
TLE line 2: 2 22455 70.8448 250.5710 0069379 44.5288 22.2490 14.59507449673841
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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