View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 19046U 88032B 24276.88352513 .00017574 00000-0 10197-2 0 9991
2 19046 97.4611 255.8925 0028580 246.3595 113.4635 15.11858851972872
| Epoch (UTC): | 02 October 2024 21:12:16 |
| Eccentricity: | 0.0028580 |
| inclination: | 97.4611° |
| perigee height: | 511 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 255.8925° |
| argument of perigee: | 246.3595° |
| revolutions per day: | 15.11858851 |
| mean anomaly at epoch: | 113.4635° |
| orbit number at epoch: | 97287 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|