| Official name | SL-16 DEB |
| Alternative name | Zenit-2 fragmentation debris |
| Cospar ID | 1992-093ES |
| Norad ID | 22453 |
| Launch date | 1992-12-25 |
| Launch site | TTMTR |
| Launch vehicle | Zenit-2 |
| RCS size | SMALL |
| Decay date | ON ORBIT |
| Period (min) | 103.71 |
| Inclination (deg) | 70.8 |
| Perigee (km) | 810 |
| Apogee (km) | 1058 |
| Eccentricity | 0.132762312633833 |
| Mean motion (revs. per day) | 13.8848712756726 |
| Semi-Major axis (km) | 7312.135 |
| Raan (deg) | 202.63 |
| Arg of perigee (deg) | 279.7175 |
GMSPAZIO serves since 2005 Aerospace, Defense, and Homeland Security, with solutions focused on 4Ds (Space + Time) Synthetic Scenarios Management to help customers managing: Complex Simulation Scenarios, Space Surveillance & Tracking and Space Situational Awareness issues, Border Patrol Control Activities, Missile Defense Network Modeling, Satellite Remote Sensing Projects, and UAVs Surveillance Activities, offering Products, Services, and Training to develop Integrated and Customized Information Systems, and customers’ tailored software applications and services.
To protect as much as possible your privacy, no authentication is required on this website, so a cookie must be used to store your favorites.
For these reasons, if you change your browser or use another device, your saved favorites will not be displayed.
If you confirm, you accept the use of the cookie to store your favorites.
.png)
