View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 06324U 72104B 25192.59545943 .00000156 00000-0 52332-4 0 9993
2 06324 74.0769 42.3378 0008270 148.4499 211.7156 14.45055771760525
| Epoch (UTC): | 11 July 2025 14:17:27 |
| Eccentricity: | 0.0008270 |
| inclination: | 74.0769° |
| perigee height: | 736 km |
| apogee height: | 748 km |
| right ascension of ascending node: | 42.3378° |
| argument of perigee: | 148.4499° |
| revolutions per day: | 14.45055771 |
| mean anomaly at epoch: | 211.7156° |
| orbit number at epoch: | 76052 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|