View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 24278U 96046B 23090.55077631 .00000047 00000-0 86530-4 0 9993
2 24278 98.5235 79.7054 0349205 258.2658 97.9113 13.53140204314683
| Epoch (UTC): | 31 March 2023 13:13:07 |
| Eccentricity: | 0.0349205 |
| inclination: | 98.5235° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 79.7054° |
| argument of perigee: | 258.2658° |
| revolutions per day: | 13.53140204 |
| mean anomaly at epoch: | 97.9113° |
| orbit number at epoch: | 31468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|