View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28470U 04044A 24278.21698817 .00014520 00000-0 84347-3 0 9999
2 28470 97.2149 89.3187 0037783 225.4617 134.3526 15.11588727 93726
| Epoch (UTC): | 04 October 2024 05:12:27 |
| Eccentricity: | 0.0037783 |
| inclination: | 97.2149° |
| perigee height: | 505 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 89.3187° |
| argument of perigee: | 225.4617° |
| revolutions per day: | 15.11588727 |
| mean anomaly at epoch: | 134.3526° |
| orbit number at epoch: | 9372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|