View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28059U 26075.87920350 +.00000000 +00000-0 +85660-4 0 00000
2 28059 98.6883 71.0664 0047568 208.5739 151.2849 14.55027043 07
| Epoch (UTC): | 16 March 2026 21:06:03 |
| Eccentricity: | 0.0047568 |
| inclination: | 98.6883° |
| perigee height: | 676 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 71.0664° |
| argument of perigee: | 208.5739° |
| revolutions per day: | 14.55027043 |
| mean anomaly at epoch: | 151.2849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|