View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 09482U 76102B 22228.36502807 .00000131 00000-0 68957-4 0 9990
2 09482 81.2586 86.3148 0078536 244.4111 114.8927 14.07604204352922
| Epoch (UTC): | 16 August 2022 08:45:38 |
| Eccentricity: | 0.0078536 |
| inclination: | 81.2586° |
| perigee height: | 810 km |
| apogee height: | 924 km |
| right ascension of ascending node: | 86.3148° |
| argument of perigee: | 244.4111° |
| revolutions per day: | 14.07604204 |
| mean anomaly at epoch: | 114.8927° |
| orbit number at epoch: | 35292 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|