View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55638U 26145.35961733 +.00000000 +00000-0 +27899-4 0 00004
2 55638 70.0000 11.1039 0002679 270.9505 89.1347 14.98331396 02
| Epoch (UTC): | 25 May 2026 08:37:50 |
| Eccentricity: | 0.0002679 |
| inclination: | 70.0000° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 11.1039° |
| argument of perigee: | 270.9505° |
| revolutions per day: | 14.98331396 |
| mean anomaly at epoch: | 89.1347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|