View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42603U 26101.48159095 +.00000000 +00000-0 +77483-3 0 00001
2 42603 100.8902 199.6135 0214820 124.9544 237.1892 12.17929692 07
| Epoch (UTC): | 11 April 2026 11:33:29 |
| Eccentricity: | 0.0214820 |
| inclination: | 100.8902° |
| perigee height: | 1430 km |
| apogee height: | 1773 km |
| right ascension of ascending node: | 199.6135° |
| argument of perigee: | 124.9544° |
| revolutions per day: | 12.17929692 |
| mean anomaly at epoch: | 237.1892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|