View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25544U 98067A 22274.70624079 -.00189013 00000-0 -34343-2 0 9995
2 25544 51.6406 168.8484 0003279 236.2875 219.6200 15.49581705361709
| Epoch (UTC): | 01 October 2022 16:56:59 |
| Eccentricity: | 0.0003279 |
| inclination: | 51.6406° |
| perigee height: | 416 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 168.8484° |
| argument of perigee: | 236.2875° |
| revolutions per day: | 15.49581705 |
| mean anomaly at epoch: | 219.6200° |
| orbit number at epoch: | 36170 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|