View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16275U 26111.96062234 +.00000000 +00000-0 +00000-0 0 00007
2 16275 13.4061 340.5379 0005188 328.5426 39.3922 0.99956056 08
| Epoch (UTC): | 21 April 2026 23:03:17 |
| Eccentricity: | 0.0005188 |
| inclination: | 13.4061° |
| perigee height: | 35853 km |
| apogee height: | 35897 km |
| right ascension of ascending node: | 340.5379° |
| argument of perigee: | 328.5426° |
| revolutions per day: | 0.99956056 |
| mean anomaly at epoch: | 39.3922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|