View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25544U 26159.80410962 +.00000000 +00000-0 +13425-3 0 00004
2 25544 51.6336 341.5878 0006923 148.5365 211.6039 15.49672912 02
| Epoch (UTC): | 08 June 2026 19:17:55 |
| Eccentricity: | 0.0006923 |
| inclination: | 51.6336° |
| perigee height: | 413 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 341.5878° |
| argument of perigee: | 148.5365° |
| revolutions per day: | 15.49672912 |
| mean anomaly at epoch: | 211.6039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|