View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55778U 26145.10949317 +.00000000 +00000-0 +20941-4 0 00007
2 55778 69.9999 31.6340 0002769 266.7907 93.2935 14.98330714 04
| Epoch (UTC): | 25 May 2026 02:37:40 |
| Eccentricity: | 0.0002769 |
| inclination: | 69.9999° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.6340° |
| argument of perigee: | 266.7907° |
| revolutions per day: | 14.98330714 |
| mean anomaly at epoch: | 93.2935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|