View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 41058U 00055R 24357.54962986 .00001986 00000-0 11189-2 0 9994
2 41058 98.5867 6.4688 0022909 251.6194 108.2486 14.11316689466482
| Epoch (UTC): | 22 December 2024 13:11:28 |
| Eccentricity: | 0.0022909 |
| inclination: | 98.5867° |
| perigee height: | 838 km |
| apogee height: | 871 km |
| right ascension of ascending node: | 6.4688° |
| argument of perigee: | 251.6194° |
| revolutions per day: | 14.11316689 |
| mean anomaly at epoch: | 108.2486° |
| orbit number at epoch: | 46648 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|