View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 44354U 19036R 22177.53672563 .00060489 -50984-5 52651-3 0 9996
2 44354 28.5229 115.3348 0226100 73.0901 289.4357 15.40994054166086
| Epoch (UTC): | 26 June 2022 12:52:53 |
| Eccentricity: | 0.0226100 |
| inclination: | 28.5229° |
| perigee height: | 289 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 115.3348° |
| argument of perigee: | 73.0901° |
| revolutions per day: | 15.40994054 |
| mean anomaly at epoch: | 289.4357° |
| orbit number at epoch: | 16608 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|