View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 47268U 20100L 24278.48949716 -.00000322 00000-0 -93116-3 0 9993
2 47268 87.8846 114.2869 0001751 84.0753 276.0575 13.12442452183138
| Epoch (UTC): | 04 October 2024 11:44:52 |
| Eccentricity: | 0.0001751 |
| inclination: | 87.8846° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 114.2869° |
| argument of perigee: | 84.0753° |
| revolutions per day: | 13.12442452 |
| mean anomaly at epoch: | 276.0575° |
| orbit number at epoch: | 18313 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|