View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 17997U 87043A 23069.78187572 0.00015500 00000-0 84221-3 0 04
2 17997 63.3371 309.2262 0913503 89.6999 270.3001 13.61555117 01
| Epoch (UTC): | 10 March 2023 18:45:54 |
| Eccentricity: | 0.0913503 |
| inclination: | 63.3371° |
| perigee height: | 353 km |
| apogee height: | 1707 km |
| right ascension of ascending node: | 309.2262° |
| argument of perigee: | 89.6999° |
| revolutions per day: | 13.61555117 |
| mean anomaly at epoch: | 270.3001° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|