View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20963U 90097B 22058.65362887 0.00000000 00000-0 00000-0 0 00
2 20963 15.6557 347.2999 0011711 240.1320 119.7636 0.98581418 04
Epoch (UTC): | 27 February 2022 15:41:13 |
Eccentricity: | 0.0011711 |
inclination: | 15.6557° |
perigee height: | 36217 km |
apogee height: | 36317 km |
right ascension of ascending node: | 347.2999° |
argument of perigee: | 240.1320° |
revolutions per day: | 0.98581418 |
mean anomaly at epoch: | 119.7636° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|