View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 36105U 09066B 24282.52956276 .00379503 00000-0 27369-2 0 9992
2 36105 97.3930 273.0924 0006796 10.8982 349.2427 15.72416561820640
| Epoch (UTC): | 08 October 2024 12:42:34 |
| Eccentricity: | 0.0006796 |
| inclination: | 97.3930° |
| perigee height: | 347 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 273.0924° |
| argument of perigee: | 10.8982° |
| revolutions per day: | 15.72416561 |
| mean anomaly at epoch: | 349.2427° |
| orbit number at epoch: | 82064 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|