View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55957U 26145.21010848 +.00000000 +00000-0 +43194-4 0 00001
2 55957 70.0002 71.5855 0003063 265.3903 94.6906 14.98332547 03
| Epoch (UTC): | 25 May 2026 05:02:33 |
| Eccentricity: | 0.0003063 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 71.5855° |
| argument of perigee: | 265.3903° |
| revolutions per day: | 14.98332547 |
| mean anomaly at epoch: | 94.6906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|