View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55954U 26145.52303984 +.00000000 +00000-0 +15164-4 0 00004
2 55954 70.0007 70.6729 0002879 270.0530 90.0299 14.98329902 04
| Epoch (UTC): | 25 May 2026 12:33:10 |
| Eccentricity: | 0.0002879 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 70.6729° |
| argument of perigee: | 270.0530° |
| revolutions per day: | 14.98329902 |
| mean anomaly at epoch: | 90.0299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|