View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 17590U 26020.27124726 +.00000000 +00000-0 -75969-4 0 00007
2 17590 71.0033 18.5225 0006254 217.9053 142.1632 14.17159457 08
| Epoch (UTC): | 20 January 2026 06:30:35 |
| Eccentricity: | 0.0006254 |
| inclination: | 71.0033° |
| perigee height: | 830 km |
| apogee height: | 839 km |
| right ascension of ascending node: | 18.5225° |
| argument of perigee: | 217.9053° |
| revolutions per day: | 14.17159457 |
| mean anomaly at epoch: | 142.1632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|