View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56627U 26014.82575497 +.00000000 +00000-0 +86264-3 0 00008
2 56627 98.8293 27.5826 0036659 27.9506 332.3628 14.19307098 04
| Epoch (UTC): | 14 January 2026 19:49:05 |
| Eccentricity: | 0.0036659 |
| inclination: | 98.8293° |
| perigee height: | 801 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 27.5826° |
| argument of perigee: | 27.9506° |
| revolutions per day: | 14.19307098 |
| mean anomaly at epoch: | 332.3628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|