View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00011U 26103.96383830 +.00000000 +00000-0 +40712-3 0 00004
2 00011 32.8672 328.2070 1444321 51.3875 320.7438 11.90348566 02
| Epoch (UTC): | 13 April 2026 23:07:55 |
| Eccentricity: | 0.1444321 |
| inclination: | 32.8672° |
| perigee height: | 554 km |
| apogee height: | 2895 km |
| right ascension of ascending node: | 328.2070° |
| argument of perigee: | 51.3875° |
| revolutions per day: | 11.90348566 |
| mean anomaly at epoch: | 320.7438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|