View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 41914U 17002B 24358.18332749 .00017848 00000-0 69323-3 0 9992
2 41914 97.2086 7.6476 0006979 328.5347 31.5473 15.26104615438926
| Epoch (UTC): | 23 December 2024 04:23:59 |
| Eccentricity: | 0.0006979 |
| inclination: | 97.2086° |
| perigee height: | 482 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 7.6476° |
| argument of perigee: | 328.5347° |
| revolutions per day: | 15.26104615 |
| mean anomaly at epoch: | 31.5473° |
| orbit number at epoch: | 43892 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|