View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 42784U 17036V 24007.80513513 .13611549 24273-5 31111-3 0 9994
2 42784 97.0806 52.5505 0008545 250.6889 109.3491 16.45962103364972
Epoch (UTC): | 07 January 2024 19:19:23 |
Eccentricity: | 0.0008545 |
inclination: | 97.0806° |
perigee height: | 144 km |
apogee height: | 155 km |
right ascension of ascending node: | 52.5505° |
argument of perigee: | 250.6889° |
revolutions per day: | 16.45962103 |
mean anomaly at epoch: | 109.3491° |
orbit number at epoch: | 36497 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|