View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 35254U 79095V 24357.39516369 .00068687 00000-0 85274-2 0 9995
2 35254 81.1951 34.0134 0002482 197.2088 162.9038 14.82244306595352
| Epoch (UTC): | 22 December 2024 09:29:02 |
| Eccentricity: | 0.0002482 |
| inclination: | 81.1951° |
| perigee height: | 620 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 34.0134° |
| argument of perigee: | 197.2088° |
| revolutions per day: | 14.82244306 |
| mean anomaly at epoch: | 162.9038° |
| orbit number at epoch: | 59535 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|