View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59808U 26145.61725051 +.00000000 +00000-0 +32364-3 0 00009
2 59808 97.3849 216.7888 0002079 329.3047 30.8065 15.16664310 03
| Epoch (UTC): | 25 May 2026 14:48:50 |
| Eccentricity: | 0.0002079 |
| inclination: | 97.3849° |
| perigee height: | 514 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 216.7888° |
| argument of perigee: | 329.3047° |
| revolutions per day: | 15.16664310 |
| mean anomaly at epoch: | 30.8065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|