View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00011U 59001A 24280.35956407 .00002025 00000-0 10639-2 0 9992
2 00011 32.8656 264.7115 1453951 138.9940 232.9611 11.88783836461741
| Epoch (UTC): | 06 October 2024 08:37:46 |
| Eccentricity: | 0.1453951 |
| inclination: | 32.8656° |
| perigee height: | 552 km |
| apogee height: | 2910 km |
| right ascension of ascending node: | 264.7115° |
| argument of perigee: | 138.9940° |
| revolutions per day: | 11.88783836 |
| mean anomaly at epoch: | 232.9611° |
| orbit number at epoch: | 46174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|