View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65335U 26145.44185941 +.00000000 +00000-0 +44690-3 0 00005
2 65335 53.1596 210.5305 0000748 66.6672 293.4407 15.30206800 05
| Epoch (UTC): | 25 May 2026 10:36:16 |
| Eccentricity: | 0.0000748 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.5305° |
| argument of perigee: | 66.6672° |
| revolutions per day: | 15.30206800 |
| mean anomaly at epoch: | 293.4407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|