View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43764U 26145.48807441 +.00000000 +00000-0 +10207-2 0 00003
2 43764 97.4170 227.7151 0004345 260.3396 99.7376 15.70967736 06
| Epoch (UTC): | 25 May 2026 11:42:49 |
| Eccentricity: | 0.0004345 |
| inclination: | 97.4170° |
| perigee height: | 353 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 227.7151° |
| argument of perigee: | 260.3396° |
| revolutions per day: | 15.70967736 |
| mean anomaly at epoch: | 99.7376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|