View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59763U 26145.39277793 +.00000000 +00000-0 +22469-4 0 00005
2 59763 53.1594 187.9036 0001294 99.2519 260.8645 15.69715937 08
| Epoch (UTC): | 25 May 2026 09:25:36 |
| Eccentricity: | 0.0001294 |
| inclination: | 53.1594° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 187.9036° |
| argument of perigee: | 99.2519° |
| revolutions per day: | 15.69715937 |
| mean anomaly at epoch: | 260.8645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|