View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00047U 60007C 22279.75726266 .00000435 00000-0 12268-3 0 9991
2 00047 66.6660 65.0858 0221117 46.4055 315.5165 14.42434378255999
| Epoch (UTC): | 06 October 2022 18:10:27 |
| Eccentricity: | 0.0221117 |
| inclination: | 66.6660° |
| perigee height: | 593 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 65.0858° |
| argument of perigee: | 46.4055° |
| revolutions per day: | 14.42434378 |
| mean anomaly at epoch: | 315.5165° |
| orbit number at epoch: | 25599 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|