View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27386U 02009A 24283.51418949 .00000901 00000-0 30752-3 0 9997
2 27386 98.2972 240.7095 0001366 90.2583 21.3049 14.38706799184944
| Epoch (UTC): | 09 October 2024 12:20:25 |
| Eccentricity: | 0.0001366 |
| inclination: | 98.2972° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 240.7095° |
| argument of perigee: | 90.2583° |
| revolutions per day: | 14.38706799 |
| mean anomaly at epoch: | 21.3049° |
| orbit number at epoch: | 18494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|