View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68584U 26145.58335647 +.00000000 +00000-0 -10163+0 0 00004
2 68584 51.8769 286.6160 0007638 303.1418 169.0859 15.21962221 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0007638 |
| inclination: | 51.8769° |
| perigee height: | 495 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 286.6160° |
| argument of perigee: | 303.1418° |
| revolutions per day: | 15.21962221 |
| mean anomaly at epoch: | 169.0859° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|