View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40613U 26145.58364176 +.00000000 +00000-0 +00000-0 0 00005
2 40613 0.0296 89.4788 0002673 327.7850 35.3634 1.00270959 04
| Epoch (UTC): | 25 May 2026 14:00:26 |
| Eccentricity: | 0.0002673 |
| inclination: | 0.0296° |
| perigee height: | 35776 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 89.4788° |
| argument of perigee: | 327.7850° |
| revolutions per day: | 1.00270959 |
| mean anomaly at epoch: | 35.3634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|