View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28480U 04046B 22147.90995205 .00000128 00000-0 64328-4 0 9999
2 28480 98.0635 137.2875 0140404 283.2649 75.2906 14.25828564911516
| Epoch (UTC): | 27 May 2022 21:50:19 |
| Eccentricity: | 0.0140404 |
| inclination: | 98.0635° |
| perigee height: | 705 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 137.2875° |
| argument of perigee: | 283.2649° |
| revolutions per day: | 14.25828564 |
| mean anomaly at epoch: | 75.2906° |
| orbit number at epoch: | 91151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|