View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 19274U 88056A 22141.87792190 .00003745 00000-0 24364-3 0 9994
2 19274 82.5043 199.8624 0008234 296.3877 63.6505 15.07691179824673
| Epoch (UTC): | 21 May 2022 21:04:12 |
| Eccentricity: | 0.0008234 |
| inclination: | 82.5043° |
| perigee height: | 537 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 199.8624° |
| argument of perigee: | 296.3877° |
| revolutions per day: | 15.07691179 |
| mean anomaly at epoch: | 63.6505° |
| orbit number at epoch: | 82467 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|