View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 30464U 99025AGB 24280.61509146 .00000679 00000-0 38711-3 0 9995
2 30464 98.9014 330.9284 0110210 38.5025 113.9538 14.09994764909738
| Epoch (UTC): | 06 October 2024 14:45:43 |
| Eccentricity: | 0.0110210 |
| inclination: | 98.9014° |
| perigee height: | 779 km |
| apogee height: | 939 km |
| right ascension of ascending node: | 330.9284° |
| argument of perigee: | 38.5025° |
| revolutions per day: | 14.09994764 |
| mean anomaly at epoch: | 113.9538° |
| orbit number at epoch: | 90973 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|