View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00011U 59001A 23080.48182127 .00003603 00000-0 19103-2 0 9991
2 00011 32.8664 232.8581 1462118 179.0775 181.2992 11.86815617394564
Epoch (UTC): | 21 March 2023 11:33:49 |
Eccentricity: | 0.1462118 |
inclination: | 32.8664° |
perigee height: | 553 km |
apogee height: | 2927 km |
right ascension of ascending node: | 232.8581° |
argument of perigee: | 179.0775° |
revolutions per day: | 11.86815617 |
mean anomaly at epoch: | 181.2992° |
orbit number at epoch: | 39456 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|