View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68497U 26145.36783265 +.00000000 +00000-0 +22733-3 0 00005
2 68497 97.7577 103.9906 0002764 60.2682 299.8812 14.92065398 05
| Epoch (UTC): | 25 May 2026 08:49:40 |
| Eccentricity: | 0.0002764 |
| inclination: | 97.7577° |
| perigee height: | 590 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 103.9906° |
| argument of perigee: | 60.2682° |
| revolutions per day: | 14.92065398 |
| mean anomaly at epoch: | 299.8812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|