View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64729U 26145.32587787 +.00000000 +00000-0 +31840-3 0 00005
2 64729 53.1578 185.1879 0001197 60.3867 299.7253 15.30199727 07
| Epoch (UTC): | 25 May 2026 07:49:15 |
| Eccentricity: | 0.0001197 |
| inclination: | 53.1578° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 185.1879° |
| argument of perigee: | 60.3867° |
| revolutions per day: | 15.30199727 |
| mean anomaly at epoch: | 299.7253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|