View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20624U 90046A 25198.30138708 -.00000242 00000-0 -10059-3 0 9996
2 20624 71.0398 153.8520 0015902 211.4912 148.5261 14.14775130814334
| Epoch (UTC): | 17 July 2025 07:13:59 |
| Eccentricity: | 0.0015902 |
| inclination: | 71.0398° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 153.8520° |
| argument of perigee: | 211.4912° |
| revolutions per day: | 14.14775130 |
| mean anomaly at epoch: | 148.5261° |
| orbit number at epoch: | 81433 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|