View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 10515U 77117B 24278.88032500 .00000463 00000-0 25999-3 0 9994
2 10515 81.2469 208.1410 0026230 268.6326 91.1840 14.08959925405000
| Epoch (UTC): | 04 October 2024 21:07:40 |
| Eccentricity: | 0.0026230 |
| inclination: | 81.2469° |
| perigee height: | 844 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 208.1410° |
| argument of perigee: | 268.6326° |
| revolutions per day: | 14.08959925 |
| mean anomaly at epoch: | 91.1840° |
| orbit number at epoch: | 40500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|