View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25979U 99064C 24357.67772904 .00015919 00000-0 83561-3 0 9994
2 25979 98.2271 28.4424 0006465 152.0692 208.0886 15.15811769361391
| Epoch (UTC): | 22 December 2024 16:15:55 |
| Eccentricity: | 0.0006465 |
| inclination: | 98.2271° |
| perigee height: | 514 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 28.4424° |
| argument of perigee: | 152.0692° |
| revolutions per day: | 15.15811769 |
| mean anomaly at epoch: | 208.0886° |
| orbit number at epoch: | 36139 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|