View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 38341U 12025E 23265.75420725 .00003393 00000-0 38046-3 0 9991
2 38341 98.4396 155.6072 0052925 358.5927 1.5130 14.86567369614284
| Epoch (UTC): | 22 September 2023 18:06:03 |
| Eccentricity: | 0.0052925 |
| inclination: | 98.4396° |
| perigee height: | 571 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 155.6072° |
| argument of perigee: | 358.5927° |
| revolutions per day: | 14.86567369 |
| mean anomaly at epoch: | 1.5130° |
| orbit number at epoch: | 61428 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|