View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25019U 97065A 25118.44711758 -.00000065 00000-0 00000-0 0 9990
2 25019 12.2892 24.7157 0003923 324.6640 276.1048 1.00272927 28795
| Epoch (UTC): | 28 April 2025 10:43:50 |
| Eccentricity: | 0.0003923 |
| inclination: | 12.2892° |
| perigee height: | 35769 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 24.7157° |
| argument of perigee: | 324.6640° |
| revolutions per day: | 1.00272927 |
| mean anomaly at epoch: | 276.1048° |
| orbit number at epoch: | 2879 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|