View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25544U 98067A 25119.19035294 .00013779 00000-0 25440-3 0 9996
2 25544 51.6352 189.7367 0002491 81.0639 279.0631 15.49383308507563
| Epoch (UTC): | 29 April 2025 04:34:06 |
| Eccentricity: | 0.0002491 |
| inclination: | 51.6352° |
| perigee height: | 417 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 189.7367° |
| argument of perigee: | 81.0639° |
| revolutions per day: | 15.49383308 |
| mean anomaly at epoch: | 279.0631° |
| orbit number at epoch: | 50756 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|