View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68301U 26145.34101903 +.00000000 +00000-0 +11078-2 0 00009
2 68301 97.2856 271.6260 0001590 48.0087 312.1313 15.75243336 06
| Epoch (UTC): | 25 May 2026 08:11:04 |
| Eccentricity: | 0.0001590 |
| inclination: | 97.2856° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.6260° |
| argument of perigee: | 48.0087° |
| revolutions per day: | 15.75243336 |
| mean anomaly at epoch: | 312.1313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|