View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 56728U 23068U 24358.16628034 .00002870 00000-0 37403-3 0 9996
2 56728 86.1985 225.7349 0002258 93.2730 266.8749 14.80244974 86335
| Epoch (UTC): | 23 December 2024 03:59:26 |
| Eccentricity: | 0.0002258 |
| inclination: | 86.1985° |
| perigee height: | 627 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 225.7349° |
| argument of perigee: | 93.2730° |
| revolutions per day: | 14.80244974 |
| mean anomaly at epoch: | 266.8749° |
| orbit number at epoch: | 8633 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|