View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00029U 60002B 23271.60550118 .00001330 00000-0 22249-3 0 9999
2 00029 48.3796 51.2567 0023891 320.3464 39.5701 14.75565104395371
| Epoch (UTC): | 28 September 2023 14:31:55 |
| Eccentricity: | 0.0023891 |
| inclination: | 48.3796° |
| perigee height: | 626 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 51.2567° |
| argument of perigee: | 320.3464° |
| revolutions per day: | 14.75565104 |
| mean anomaly at epoch: | 39.5701° |
| orbit number at epoch: | 39537 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|