View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64794U 26145.40679792 +.00000000 +00000-0 -20210-4 0 00005
2 64794 70.0008 301.2133 0002426 271.1539 88.9343 14.98326019 00
| Epoch (UTC): | 25 May 2026 09:45:47 |
| Eccentricity: | 0.0002426 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 301.2133° |
| argument of perigee: | 271.1539° |
| revolutions per day: | 14.98326019 |
| mean anomaly at epoch: | 88.9343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|