View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27601U 02056E 24284.45086424 .00001791 00000-0 65062-3 0 9992
2 27601 98.2455 255.8967 0069506 257.6323 215.6759 14.33087968140297
| Epoch (UTC): | 10 October 2024 10:49:14 |
| Eccentricity: | 0.0069506 |
| inclination: | 98.2455° |
| perigee height: | 731 km |
| apogee height: | 831 km |
| right ascension of ascending node: | 255.8967° |
| argument of perigee: | 257.6323° |
| revolutions per day: | 14.33087968 |
| mean anomaly at epoch: | 215.6759° |
| orbit number at epoch: | 14029 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|