View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 21949U 92023A 23125.13420956 0.00000243 00000-0 91301-4 0 04
2 21949 85.0128 10.9231 0002118 112.5366 247.4581 14.31668183 05
| Epoch (UTC): | 05 May 2023 03:13:15 |
| Eccentricity: | 0.0002118 |
| inclination: | 85.0128° |
| perigee height: | 784 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 10.9231° |
| argument of perigee: | 112.5366° |
| revolutions per day: | 14.31668183 |
| mean anomaly at epoch: | 247.4581° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|