View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63905U 26145.25779213 +.00000000 +00000-0 +48945-3 0 00003
2 63905 43.0013 104.1727 0001013 269.2904 90.7831 15.27590910 02
| Epoch (UTC): | 25 May 2026 06:11:13 |
| Eccentricity: | 0.0001013 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 104.1727° |
| argument of perigee: | 269.2904° |
| revolutions per day: | 15.27590910 |
| mean anomaly at epoch: | 90.7831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|