View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62743U 26145.52622713 +.00000000 +00000-0 +75470-3 0 00007
2 62743 42.9970 87.8003 0000808 252.8518 107.2245 15.27590744 03
| Epoch (UTC): | 25 May 2026 12:37:46 |
| Eccentricity: | 0.0000808 |
| inclination: | 42.9970° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.8003° |
| argument of perigee: | 252.8518° |
| revolutions per day: | 15.27590744 |
| mean anomaly at epoch: | 107.2245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|