View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56344U 26145.47039936 +.00000000 +00000-0 +26658-3 0 00004
2 56344 97.4456 146.5809 0002061 84.6003 275.5459 15.05644171 03
| Epoch (UTC): | 25 May 2026 11:17:22 |
| Eccentricity: | 0.0002061 |
| inclination: | 97.4456° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.5809° |
| argument of perigee: | 84.6003° |
| revolutions per day: | 15.05644171 |
| mean anomaly at epoch: | 275.5459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|