View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65955U 26145.37548471 +.00000000 +00000-0 +11792-3 0 00003
2 65955 51.9007 21.4916 0000716 103.1015 257.0027 14.79934695 02
| Epoch (UTC): | 25 May 2026 09:00:41 |
| Eccentricity: | 0.0000716 |
| inclination: | 51.9007° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 21.4916° |
| argument of perigee: | 103.1015° |
| revolutions per day: | 14.79934695 |
| mean anomaly at epoch: | 257.0027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|