View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 01778U 26156.68588838 +.00000000 +00000-0 +21338-3 0 00000
2 01778 34.2553 290.2130 0738771 118.1163 249.6134 13.49801530 01
| Epoch (UTC): | 05 June 2026 16:27:40 |
| Eccentricity: | 0.0738771 |
| inclination: | 34.2553° |
| perigee height: | 523 km |
| apogee height: | 1623 km |
| right ascension of ascending node: | 290.2130° |
| argument of perigee: | 118.1163° |
| revolutions per day: | 13.49801530 |
| mean anomaly at epoch: | 249.6134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|