View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21263U 26074.57429919 +.00000000 +00000-0 +58396-4 0 00007
2 21263 98.6160 64.4840 0012684 304.9408 55.0581 14.26719634 08
| Epoch (UTC): | 15 March 2026 13:46:59 |
| Eccentricity: | 0.0012684 |
| inclination: | 98.6160° |
| perigee height: | 794 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 64.4840° |
| argument of perigee: | 304.9408° |
| revolutions per day: | 14.26719634 |
| mean anomaly at epoch: | 55.0581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|