View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 35117U 99025DKV 22269.04677384 .00007061 00000-0 21994-2 0 9993
2 35117 98.7574 20.2944 0051835 159.0055 201.3276 14.40434535485828
| Epoch (UTC): | 26 September 2022 01:07:21 |
| Eccentricity: | 0.0051835 |
| inclination: | 98.7574° |
| perigee height: | 720 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 20.2944° |
| argument of perigee: | 159.0055° |
| revolutions per day: | 14.40434535 |
| mean anomaly at epoch: | 201.3276° |
| orbit number at epoch: | 48582 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|