View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 32480U 26065.52699339 +.00000000 +00000-0 +17293-2 0 00009
2 32480 45.1137 158.2072 6987715 34.8730 355.3134 2.30096766 06
| Epoch (UTC): | 06 March 2026 12:38:52 |
| Eccentricity: | 0.6987715 |
| inclination: | 45.1137° |
| perigee height: | 922 km |
| apogee height: | 34793 km |
| right ascension of ascending node: | 158.2072° |
| argument of perigee: | 34.8730° |
| revolutions per day: | 2.30096766 |
| mean anomaly at epoch: | 355.3134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|