| SPACE OBJECT | Back to the directory |
|---|
| registration | 2019-B-SC-033 |
| designation | QARMAN |
| operator | VON KARMAN INSTITUTE |
| owner(s) | VON KARMAN INSTITUTE |
| type | cubesat |
| mission/function | Study of the use of cubesats as atmosphere re-entry vehicle |
| nodal period (min) | 92,68 |
| inclination (deg) | 51,64 |
| perigee (km) | 408 |
| apogee (km) | 410 |
| radiofrequencies | 437.35 MHz
|
| GSO position | No |
| autonomous maneuvrability in orbit | No |
| update | The object re-entered the atmosphere on 05/02/2012 (14.41h UTC).
The re-entry was nominal and caused the complete disintegration of the object. |
| launch service provider | SpaceX (Etats-Unis - Verenigde Staten - United States) (Falcon 9) |
| launch location and facility | Hawthorne, CA (Etats-Unis - Verenigde Staten - United States) |
| positioning location and facility | ISS |
| other launching State(s) | Etats-Unis - Verenigde Staten - United States |
| date and time of launching (UTC) | 04/12/2019 17:29:00 |
| positioning | 19/02/2020 11:20:00 |
| national authorization date | 20/11/2019 |
| national authorization number | 2019/01 |
| national registry inscription | 26/11/2019 |
| notification to UNOOSA | 25/02/2020 |
| notes | |
