View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58913U 26145.37785175 +.00000000 +00000-0 +19603-3 0 00002
2 58913 50.0033 99.7883 0022223 280.6269 79.2167 14.83142646 08
| Epoch (UTC): | 25 May 2026 09:04:06 |
| Eccentricity: | 0.0022223 |
| inclination: | 50.0033° |
| perigee height: | 604 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 99.7883° |
| argument of perigee: | 280.6269° |
| revolutions per day: | 14.83142646 |
| mean anomaly at epoch: | 79.2167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|