View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25396U 98043C 22222.14659086 .00000064 00000-0 46705-4 0 9994
2 25396 98.7976 172.1356 0001491 270.4329 89.6679 14.24677670251838
| Epoch (UTC): | 10 August 2022 03:31:05 |
| Eccentricity: | 0.0001491 |
| inclination: | 98.7976° |
| perigee height: | 808 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 172.1356° |
| argument of perigee: | 270.4329° |
| revolutions per day: | 14.24677670 |
| mean anomaly at epoch: | 89.6679° |
| orbit number at epoch: | 25183 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|