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 23080.11229049 .00000748 00000-0 18600-3 0 9992
2 00047 66.6675 342.6172 0233281 286.1602 71.3942 14.42741043279844
| Epoch (UTC): | 21 March 2023 02:41:41 |
| Eccentricity: | 0.0233281 |
| inclination: | 66.6675° |
| perigee height: | 583 km |
| apogee height: | 916 km |
| right ascension of ascending node: | 342.6172° |
| argument of perigee: | 286.1602° |
| revolutions per day: | 14.42741043 |
| mean anomaly at epoch: | 71.3942° |
| orbit number at epoch: | 27984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|