View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68772U 26145.58335647 +.00000000 +00000-0 -57293-1 0 00000
2 68772 97.2851 182.3905 0001404 99.7410 285.9025 15.51629061 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001404 |
| inclination: | 97.2851° |
| perigee height: | 411 km |
| apogee height: | 413 km |
| right ascension of ascending node: | 182.3905° |
| argument of perigee: | 99.7410° |
| revolutions per day: | 15.51629061 |
| mean anomaly at epoch: | 285.9025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|