View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 21805U 91080B 24284.23848501 .00000030 00000-0 00000-0 0 9998
2 21805 14.3397 349.8996 0005642 126.3539 239.6363 0.99184115 19616
| Epoch (UTC): | 10 October 2024 05:43:25 |
| Eccentricity: | 0.0005642 |
| inclination: | 14.3397° |
| perigee height: | 36070 km |
| apogee height: | 36118 km |
| right ascension of ascending node: | 349.8996° |
| argument of perigee: | 126.3539° |
| revolutions per day: | 0.99184115 |
| mean anomaly at epoch: | 239.6363° |
| orbit number at epoch: | 1961 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|