View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59360U 26145.50238763 +.00000000 +00000-0 +17731-4 0 00001
2 59360 43.0032 185.7801 0001542 280.0806 79.9872 15.27576931 01
| Epoch (UTC): | 25 May 2026 12:03:26 |
| Eccentricity: | 0.0001542 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.7801° |
| argument of perigee: | 280.0806° |
| revolutions per day: | 15.27576931 |
| mean anomaly at epoch: | 79.9872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|