View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00011U 59001A 23030.48547463 .00001734 00000-0 90842-3 0 9997
2 00011 32.8795 60.8527 1463595 256.3493 87.0395 11.86434308388628
| Epoch (UTC): | 30 January 2023 11:39:05 |
| Eccentricity: | 0.1463595 |
| inclination: | 32.8795° |
| perigee height: | 553 km |
| apogee height: | 2930 km |
| right ascension of ascending node: | 60.8527° |
| argument of perigee: | 256.3493° |
| revolutions per day: | 11.86434308 |
| mean anomaly at epoch: | 87.0395° |
| orbit number at epoch: | 38862 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|