View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 16117U 85092C 24283.63793434 -.00000132 00000-0 00000-0 0 9995
2 16117 14.6044 350.7623 0007055 139.6284 225.0466 0.98988871 19635
| Epoch (UTC): | 09 October 2024 15:18:37 |
| Eccentricity: | 0.0007055 |
| inclination: | 14.6044° |
| perigee height: | 36120 km |
| apogee height: | 36180 km |
| right ascension of ascending node: | 350.7623° |
| argument of perigee: | 139.6284° |
| revolutions per day: | 0.98988871 |
| mean anomaly at epoch: | 225.0466° |
| orbit number at epoch: | 1963 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|