View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45081U 26145.63444730 +.00000000 +00000-0 +46606-3 0 00005
2 45081 53.0490 219.0651 0003503 326.2978 33.7818 15.75703292 04
| Epoch (UTC): | 25 May 2026 15:13:36 |
| Eccentricity: | 0.0003503 |
| inclination: | 53.0490° |
| perigee height: | 340 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 219.0651° |
| argument of perigee: | 326.2978° |
| revolutions per day: | 15.75703292 |
| mean anomaly at epoch: | 33.7818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|