View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 15593U 85020B 25191.56454646 .00000300 00000-0 31103-4 0 9991
2 15593 82.5361 24.3935 0011928 31.2485 328.9438 14.86490673160237
| Epoch (UTC): | 10 July 2025 13:32:56 |
| Eccentricity: | 0.0011928 |
| inclination: | 82.5361° |
| perigee height: | 600 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 24.3935° |
| argument of perigee: | 31.2485° |
| revolutions per day: | 14.86490673 |
| mean anomaly at epoch: | 328.9438° |
| orbit number at epoch: | 16023 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|