View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 33498U 09002G 24357.76560959 .00007166 00000-0 76397-3 0 9991
2 33498 98.1196 276.1483 0009838 142.7398 217.4503 14.89155257857702
| Epoch (UTC): | 22 December 2024 18:22:28 |
| Eccentricity: | 0.0009838 |
| inclination: | 98.1196° |
| perigee height: | 594 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 276.1483° |
| argument of perigee: | 142.7398° |
| revolutions per day: | 14.89155257 |
| mean anomaly at epoch: | 217.4503° |
| orbit number at epoch: | 85770 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|