View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39205U 13035D 24357.85716047 .00011574 00000-0 16598-2 0 9999
2 39205 97.8051 357.8907 0071199 128.5905 232.1711 14.74916591608027
| Epoch (UTC): | 22 December 2024 20:34:18 |
| Eccentricity: | 0.0071199 |
| inclination: | 97.8051° |
| perigee height: | 595 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 357.8907° |
| argument of perigee: | 128.5905° |
| revolutions per day: | 14.74916591 |
| mean anomaly at epoch: | 232.1711° |
| orbit number at epoch: | 60802 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|