View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46460U 26145.56422472 +.00000000 +00000-0 +68508-3 0 00003
2 46460 97.2252 198.0391 0007923 83.5691 276.6471 15.64320077 01
| Epoch (UTC): | 25 May 2026 13:32:29 |
| Eccentricity: | 0.0007923 |
| inclination: | 97.2252° |
| perigee height: | 370 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 198.0391° |
| argument of perigee: | 83.5691° |
| revolutions per day: | 15.64320077 |
| mean anomaly at epoch: | 276.6471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|