View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56491U 26145.40436913 +.00000000 +00000-0 +47392-3 0 00004
2 56491 69.9990 271.0255 0003184 269.6895 90.3899 14.98317538 09
| Epoch (UTC): | 25 May 2026 09:42:17 |
| Eccentricity: | 0.0003184 |
| inclination: | 69.9990° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 271.0255° |
| argument of perigee: | 269.6895° |
| revolutions per day: | 14.98317538 |
| mean anomaly at epoch: | 90.3899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|