View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59711U 26145.18224146 +.00000000 +00000-0 +11236-4 0 00009
2 59711 53.1585 309.3822 0001068 84.6842 275.4298 15.69706896 00
| Epoch (UTC): | 25 May 2026 04:22:25 |
| Eccentricity: | 0.0001068 |
| inclination: | 53.1585° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 309.3822° |
| argument of perigee: | 84.6842° |
| revolutions per day: | 15.69706896 |
| mean anomaly at epoch: | 275.4298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|