View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59035U 26145.48703795 +.00000000 +00000-0 +70997-4 0 00002
2 59035 42.9992 309.8333 0000683 285.5432 74.5345 15.27579273 00
| Epoch (UTC): | 25 May 2026 11:41:20 |
| Eccentricity: | 0.0000683 |
| inclination: | 42.9992° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.8333° |
| argument of perigee: | 285.5432° |
| revolutions per day: | 15.27579273 |
| mean anomaly at epoch: | 74.5345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|