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 22176.38262890 .00000183 00000-0 57922-4 0 9996
2 00029 48.3806 65.5786 0023703 150.8207 209.4034 14.74661788327430
| Epoch (UTC): | 25 June 2022 09:10:59 |
| Eccentricity: | 0.0023703 |
| inclination: | 48.3806° |
| perigee height: | 629 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 65.5786° |
| argument of perigee: | 150.8207° |
| revolutions per day: | 14.74661788 |
| mean anomaly at epoch: | 209.4034° |
| orbit number at epoch: | 32743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|