View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60065U 26145.34502421 +.00000000 +00000-0 +28299-4 0 00003
2 60065 53.1591 173.1179 0001105 79.3441 280.7702 15.69695625 07
| Epoch (UTC): | 25 May 2026 08:16:50 |
| Eccentricity: | 0.0001105 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 173.1179° |
| argument of perigee: | 79.3441° |
| revolutions per day: | 15.69695625 |
| mean anomaly at epoch: | 280.7702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|