View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68190U 26145.34423902 +.00000000 +00000-0 +11088-2 0 00002
2 68190 53.1604 270.3827 0001143 86.5566 273.5567 15.34411033 09
| Epoch (UTC): | 25 May 2026 08:15:42 |
| Eccentricity: | 0.0001143 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 270.3827° |
| argument of perigee: | 86.5566° |
| revolutions per day: | 15.34411033 |
| mean anomaly at epoch: | 273.5567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|