View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46796U 26145.58335647 +.00000000 +00000-0 +78449-3 0 00009
2 46796 53.0391 248.8940 0005620 305.5355 324.1587 15.82395561 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0005620 |
| inclination: | 53.0391° |
| perigee height: | 320 km |
| apogee height: | 327 km |
| right ascension of ascending node: | 248.8940° |
| argument of perigee: | 305.5355° |
| revolutions per day: | 15.82395561 |
| mean anomaly at epoch: | 324.1587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|