View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68069U 26145.39349701 +.00000000 +00000-0 +54064-3 0 00008
2 68069 53.1579 182.1118 0001112 77.6889 282.4238 15.34403232 09
| Epoch (UTC): | 25 May 2026 09:26:38 |
| Eccentricity: | 0.0001112 |
| inclination: | 53.1579° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 182.1118° |
| argument of perigee: | 77.6889° |
| revolutions per day: | 15.34403232 |
| mean anomaly at epoch: | 282.4238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|