View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 40910U 15049M 24092.20923921 .16747303 26701-5 28112-3 0 9997
2 40910 97.4046 122.6776 0010391 231.3491 128.6883 16.47481859473951
Epoch (UTC): | 01 April 2024 05:01:18 |
Eccentricity: | 0.0010391 |
inclination: | 97.4046° |
perigee height: | 139 km |
apogee height: | 153 km |
right ascension of ascending node: | 122.6776° |
argument of perigee: | 231.3491° |
revolutions per day: | 16.47481859 |
mean anomaly at epoch: | 128.6883° |
orbit number at epoch: | 47395 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|