View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45564U 26145.49104174 +.00000000 +00000-0 +82786-3 0 00009
2 45564 53.0459 64.9232 0003017 56.6708 303.4591 15.55977519 00
| Epoch (UTC): | 25 May 2026 11:47:06 |
| Eccentricity: | 0.0003017 |
| inclination: | 53.0459° |
| perigee height: | 397 km |
| apogee height: | 401 km |
| right ascension of ascending node: | 64.9232° |
| argument of perigee: | 56.6708° |
| revolutions per day: | 15.55977519 |
| mean anomaly at epoch: | 303.4591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|