View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65238U 26145.07325174 +.00000000 +00000-0 -39304-5 0 00009
2 65238 97.4504 187.9205 0001493 126.0333 234.1032 15.05646660 06
| Epoch (UTC): | 25 May 2026 01:45:28 |
| Eccentricity: | 0.0001493 |
| inclination: | 97.4504° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 187.9205° |
| argument of perigee: | 126.0333° |
| revolutions per day: | 15.05646660 |
| mean anomaly at epoch: | 234.1032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|