View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28500U 04050A 23087.86125317 -.00000125 00000-0 00000-0 0 9996
2 28500 16.0016 335.3186 2785620 308.2165 263.8570 1.41309673 94261
| Epoch (UTC): | 28 March 2023 20:40:12 |
| Eccentricity: | 0.2785620 |
| inclination: | 16.0016° |
| perigee height: | 17822 km |
| apogee height: | 36510 km |
| right ascension of ascending node: | 335.3186° |
| argument of perigee: | 308.2165° |
| revolutions per day: | 1.41309673 |
| mean anomaly at epoch: | 263.8570° |
| orbit number at epoch: | 9426 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|