View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61694U 26145.34382703 +.00000000 +00000-0 +70052-5 0 00006
2 61694 53.1591 8.3351 0000881 118.3256 241.7851 15.69708040 03
| Epoch (UTC): | 25 May 2026 08:15:06 |
| Eccentricity: | 0.0000881 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 8.3351° |
| argument of perigee: | 118.3256° |
| revolutions per day: | 15.69708040 |
| mean anomaly at epoch: | 241.7851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|