View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60068U 26145.45774983 +.00000000 +00000-0 +63235-5 0 00002
2 60068 53.1592 173.1258 0001138 74.2963 285.8180 15.69703288 09
| Epoch (UTC): | 25 May 2026 10:59:09 |
| Eccentricity: | 0.0001138 |
| inclination: | 53.1592° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 173.1258° |
| argument of perigee: | 74.2963° |
| revolutions per day: | 15.69703288 |
| mean anomaly at epoch: | 285.8180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|