View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20U 59007A 24252.18399286 .00005822 00000-0 23300-2 0 9991
2 20 33.3463 72.5990 1648722 190.5600 165.5804 11.59652612409436
| Epoch (UTC): | 08 September 2024 04:24:56 |
| Eccentricity: | 0.1648722 |
| inclination: | 33.3463° |
| perigee height: | 507 km |
| apogee height: | 3226 km |
| right ascension of ascending node: | 72.5990° |
| argument of perigee: | 190.5600° |
| revolutions per day: | 11.59652612 |
| mean anomaly at epoch: | 165.5804° |
| orbit number at epoch: | 40943 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|