View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 11416U 79057A 25344.32626291 .00000536 00000-0 20200-3 0 9991
2 11416 98.5839 9.9897 0010952 97.8602 262.3827 14.35351096423868
| Epoch (UTC): | 10 December 2025 07:49:49 |
| Eccentricity: | 0.0010952 |
| inclination: | 98.5839° |
| perigee height: | 766 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 9.9897° |
| argument of perigee: | 97.8602° |
| revolutions per day: | 14.35351096 |
| mean anomaly at epoch: | 262.3827° |
| orbit number at epoch: | 42386 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|