View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40555U 26145.62440352 +.00000000 +00000-0 +68896-4 0 00007
2 40555 82.5176 248.7337 0607466 335.7692 21.5940 13.61376438 01
| Epoch (UTC): | 25 May 2026 14:59:08 |
| Eccentricity: | 0.0607466 |
| inclination: | 82.5176° |
| perigee height: | 581 km |
| apogee height: | 1481 km |
| right ascension of ascending node: | 248.7337° |
| argument of perigee: | 335.7692° |
| revolutions per day: | 13.61376438 |
| mean anomaly at epoch: | 21.5940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|