View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10521U 26159.51811791 +.00000000 +00000-0 +10087-3 0 00007
2 10521 74.0269 314.9166 0021126 249.5590 110.3298 14.42442578 00
| Epoch (UTC): | 08 June 2026 12:26:05 |
| Eccentricity: | 0.0021126 |
| inclination: | 74.0269° |
| perigee height: | 735 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 314.9166° |
| argument of perigee: | 249.5590° |
| revolutions per day: | 14.42442578 |
| mean anomaly at epoch: | 110.3298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|