View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 44619U 18048F 24280.92693635 .00024482 00000-0 23801-2 0 9990
2 44619 98.2775 77.6827 0016325 87.6495 272.6591 14.92463001339015
| Epoch (UTC): | 06 October 2024 22:14:47 |
| Eccentricity: | 0.0016325 |
| inclination: | 98.2775° |
| perigee height: | 579 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 77.6827° |
| argument of perigee: | 87.6495° |
| revolutions per day: | 14.92463001 |
| mean anomaly at epoch: | 272.6591° |
| orbit number at epoch: | 33901 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|