View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68174U 26144.68236314 +.00000000 +00000-0 +62399-3 0 00001
2 68174 53.1603 273.3681 0001134 78.3879 281.7250 15.34399428 00
| Epoch (UTC): | 24 May 2026 16:22:36 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 273.3681° |
| argument of perigee: | 78.3879° |
| revolutions per day: | 15.34399428 |
| mean anomaly at epoch: | 281.7250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|