View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00022U 59009A 22147.92083660 .00004809 00000-0 36580-3 0 9993
2 00022 50.2833 10.5583 0135170 91.6883 269.9552 14.96886045576558
| Epoch (UTC): | 27 May 2022 22:06:00 |
| Eccentricity: | 0.0135170 |
| inclination: | 50.2833° |
| perigee height: | 482 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 10.5583° |
| argument of perigee: | 91.6883° |
| revolutions per day: | 14.96886045 |
| mean anomaly at epoch: | 269.9552° |
| orbit number at epoch: | 57655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|