View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68565U 26145.03178939 +.00000000 +00000-0 +86873-3 0 00006
2 68565 53.1587 7.2093 0001134 84.6978 275.4154 15.34401026 07
| Epoch (UTC): | 25 May 2026 00:45:46 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 7.2093° |
| argument of perigee: | 84.6978° |
| revolutions per day: | 15.34401026 |
| mean anomaly at epoch: | 275.4154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|