View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27945U 03042G 23272.34892359 .00000992 00000-0 19116-3 0 9996
2 27945 98.2575 50.1800 0011275 208.9521 151.1058 14.65737373 68621
| Epoch (UTC): | 29 September 2023 08:22:26 |
| Eccentricity: | 0.0011275 |
| inclination: | 98.2575° |
| perigee height: | 667 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 50.1800° |
| argument of perigee: | 208.9521° |
| revolutions per day: | 14.65737373 |
| mean anomaly at epoch: | 151.1058° |
| orbit number at epoch: | 6862 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|