View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59961U 26145.48304779 +.00000000 +00000-0 +18748-4 0 00005
2 59961 53.1609 68.8471 0001215 90.3677 269.7463 15.30196297 01
| Epoch (UTC): | 25 May 2026 11:35:35 |
| Eccentricity: | 0.0001215 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 68.8471° |
| argument of perigee: | 90.3677° |
| revolutions per day: | 15.30196297 |
| mean anomaly at epoch: | 269.7463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|