View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 17590U 87027B 24281.44156279 .00000132 00000-0 89272-4 0 9999
2 17590 71.0015 288.4642 0006005 215.4673 144.6052 14.17023485942193
| Epoch (UTC): | 07 October 2024 10:35:51 |
| Eccentricity: | 0.0006005 |
| inclination: | 71.0015° |
| perigee height: | 831 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 288.4642° |
| argument of perigee: | 215.4673° |
| revolutions per day: | 14.17023485 |
| mean anomaly at epoch: | 144.6052° |
| orbit number at epoch: | 94219 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|