View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26486U 00051D 23264.99808007 .00000010 00000-0 00000-0 0 9991
2 26486 63.1264 306.7908 7377715 276.6406 253.7943 1.45765278122677
Epoch (UTC): | 21 September 2023 23:57:14 |
Eccentricity: | 0.7377715 |
inclination: | 63.1264° |
perigee height: | 2238 km |
apogee height: | 50720 km |
right ascension of ascending node: | 306.7908° |
argument of perigee: | 276.6406° |
revolutions per day: | 1.45765278 |
mean anomaly at epoch: | 253.7943° |
orbit number at epoch: | 12267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|