View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26880U 01033A 23088.16924253 -.00000300 00000-0 00000-0 0 9998
2 26880 11.6835 24.0482 0001500 345.4961 188.5722 1.00269102 21173
| Epoch (UTC): | 29 March 2023 04:03:42 |
| Eccentricity: | 0.0001500 |
| inclination: | 11.6835° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 24.0482° |
| argument of perigee: | 345.4961° |
| revolutions per day: | 1.00269102 |
| mean anomaly at epoch: | 188.5722° |
| orbit number at epoch: | 2117 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|