View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25398U 26088.18343830 +.00000000 +00000-0 +22241-4 0 00009
2 25398 99.0093 72.3577 0002377 84.5366 275.6083 14.23048498 05
| Epoch (UTC): | 29 March 2026 04:24:09 |
| Eccentricity: | 0.0002377 |
| inclination: | 99.0093° |
| perigee height: | 813 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 72.3577° |
| argument of perigee: | 84.5366° |
| revolutions per day: | 14.23048498 |
| mean anomaly at epoch: | 275.6083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|