View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 19573U 88093A 25193.86674194 .00005430 00000-0 22705-3 0 9999
2 19573 82.5229 357.4588 0011519 299.7889 60.2201 15.23327489982839
| Epoch (UTC): | 12 July 2025 20:48:06 |
| Eccentricity: | 0.0011519 |
| inclination: | 82.5229° |
| perigee height: | 488 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 357.4588° |
| argument of perigee: | 299.7889° |
| revolutions per day: | 15.23327489 |
| mean anomaly at epoch: | 60.2201° |
| orbit number at epoch: | 98283 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|