View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00016U 58002A 24253.60881723 .00000835 00000-0 11093-2 0 9995
2 00016 34.2834 12.0418 2025982 274.3384 62.9857 10.49407386621084
| Epoch (UTC): | 09 September 2024 14:36:41 |
| Eccentricity: | 0.2025982 |
| inclination: | 34.2834° |
| perigee height: | 649 km |
| apogee height: | 4220 km |
| right ascension of ascending node: | 12.0418° |
| argument of perigee: | 274.3384° |
| revolutions per day: | 10.49407386 |
| mean anomaly at epoch: | 62.9857° |
| orbit number at epoch: | 62108 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|