View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 32790U 26104.21123852 +.00000000 +00000-0 +18791-3 0 00000
2 32790 97.8607 82.7854 0008769 258.8624 101.1616 15.05166760 02
| Epoch (UTC): | 14 April 2026 05:04:11 |
| Eccentricity: | 0.0008769 |
| inclination: | 97.8607° |
| perigee height: | 545 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 82.7854° |
| argument of perigee: | 258.8624° |
| revolutions per day: | 15.05166760 |
| mean anomaly at epoch: | 101.1616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|