View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59122U 26145.58113623 +.00000000 +00000-0 +35292-3 0 00003
2 59122 97.5417 285.5033 0005722 318.7138 41.3669 15.30034158 06
| Epoch (UTC): | 25 May 2026 13:56:50 |
| Eccentricity: | 0.0005722 |
| inclination: | 97.5417° |
| perigee height: | 472 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 285.5033° |
| argument of perigee: | 318.7138° |
| revolutions per day: | 15.30034158 |
| mean anomaly at epoch: | 41.3669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|