View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45697U 26145.31994987 +.00000000 +00000-0 +46196-3 0 00001
2 45697 53.0445 8.8224 0005281 105.1682 254.9917 15.64964227 00
| Epoch (UTC): | 25 May 2026 07:40:43 |
| Eccentricity: | 0.0005281 |
| inclination: | 53.0445° |
| perigee height: | 370 km |
| apogee height: | 377 km |
| right ascension of ascending node: | 8.8224° |
| argument of perigee: | 105.1682° |
| revolutions per day: | 15.64964227 |
| mean anomaly at epoch: | 254.9917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|