View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13553U 26075.59573264 +.00000000 +00000-0 +44654-4 0 00008
2 13553 82.5682 134.9401 0018776 278.9297 247.3834 14.86672985 02
| Epoch (UTC): | 16 March 2026 14:17:51 |
| Eccentricity: | 0.0018776 |
| inclination: | 82.5682° |
| perigee height: | 595 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 134.9401° |
| argument of perigee: | 278.9297° |
| revolutions per day: | 14.86672985 |
| mean anomaly at epoch: | 247.3834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|