View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 05435U 26105.91368406 +.00000000 +00000-0 +67910-4 0 00008
2 05435 50.1407 342.7699 0101879 309.8023 49.3972 14.60209602 01
| Epoch (UTC): | 15 April 2026 21:55:42 |
| Eccentricity: | 0.0101879 |
| inclination: | 50.1407° |
| perigee height: | 620 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 342.7699° |
| argument of perigee: | 309.8023° |
| revolutions per day: | 14.60209602 |
| mean anomaly at epoch: | 49.3972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|