View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 29522U 06050A 18046.74664981 0.00000060 00000-0 31614-4 0 03
2 29522 98.8471 63.9494 0011000 72.0020 287.9979 14.13981388 04
| Epoch (UTC): | 15 February 2018 17:55:10 |
| Eccentricity: | 0.0011000 |
| inclination: | 98.8471° |
| perigee height: | 838 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 63.9494° |
| argument of perigee: | 72.0020° |
| revolutions per day: | 14.13981388 |
| mean anomaly at epoch: | 287.9979° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|