View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 22220U 92076B 25188.64317363 .00000016 00000-0 31633-4 0 9996
2 22220 71.0010 344.5399 0010839 112.4543 323.1011 14.16807716687123
| Epoch (UTC): | 07 July 2025 15:26:10 |
| Eccentricity: | 0.0010839 |
| inclination: | 71.0010° |
| perigee height: | 828 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 344.5399° |
| argument of perigee: | 112.4543° |
| revolutions per day: | 14.16807716 |
| mean anomaly at epoch: | 323.1011° |
| orbit number at epoch: | 68712 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|