View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65935U 26145.48484745 +.00000000 +00000-0 +17289-2 0 00002
2 65935 53.1575 169.1263 0000904 335.7933 24.3025 15.30231953 08
| Epoch (UTC): | 25 May 2026 11:38:10 |
| Eccentricity: | 0.0000904 |
| inclination: | 53.1575° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.1263° |
| argument of perigee: | 335.7933° |
| revolutions per day: | 15.30231953 |
| mean anomaly at epoch: | 24.3025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|