View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59716U 26145.48095983 +.00000000 +00000-0 +46271-4 0 00009
2 59716 53.1572 307.6786 0001176 69.6687 290.4458 15.69724468 01
| Epoch (UTC): | 25 May 2026 11:32:34 |
| Eccentricity: | 0.0001176 |
| inclination: | 53.1572° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 307.6786° |
| argument of perigee: | 69.6687° |
| revolutions per day: | 15.69724468 |
| mean anomaly at epoch: | 290.4458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|