View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26266U 99057FC 24358.14092618 .00010580 00000-0 19269-2 0 9998
2 26266 98.4482 70.0910 0081250 336.8457 22.9092 14.64108826303783
| Epoch (UTC): | 23 December 2024 03:22:56 |
| Eccentricity: | 0.0081250 |
| inclination: | 98.4482° |
| perigee height: | 622 km |
| apogee height: | 737 km |
| right ascension of ascending node: | 70.0910° |
| argument of perigee: | 336.8457° |
| revolutions per day: | 14.64108826 |
| mean anomaly at epoch: | 22.9092° |
| orbit number at epoch: | 30378 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|