View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 40617U 15023A 22143.90404764 .00000095 00000-0 00000+0 0 9998
2 40617 0.0310 96.4637 0002508 335.0143 187.4704 1.00270663 25938
| Epoch (UTC): | 23 May 2022 21:41:49 |
| Eccentricity: | 0.0002508 |
| inclination: | 0.0310° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 96.4637° |
| argument of perigee: | 335.0143° |
| revolutions per day: | 1.00270663 |
| mean anomaly at epoch: | 187.4704° |
| orbit number at epoch: | 2593 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|