View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64927U 26144.98708500 +.00000000 +00000-0 +56105-3 0 00005
2 64927 53.1588 351.3772 0001120 79.8981 280.2147 15.30213779 06
| Epoch (UTC): | 24 May 2026 23:41:24 |
| Eccentricity: | 0.0001120 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.3772° |
| argument of perigee: | 79.8981° |
| revolutions per day: | 15.30213779 |
| mean anomaly at epoch: | 280.2147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|