View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60491U 26145.15038925 +.00000000 +00000-0 +19914-2 0 00000
2 60491 97.3696 229.7493 0001613 127.3138 232.8263 15.54480770 01
| Epoch (UTC): | 25 May 2026 03:36:33 |
| Eccentricity: | 0.0001613 |
| inclination: | 97.3696° |
| perigee height: | 403 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 229.7493° |
| argument of perigee: | 127.3138° |
| revolutions per day: | 15.54480770 |
| mean anomaly at epoch: | 232.8263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|