View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00047U 60007C 25166.69760558 .00000339 00000-0 97816-4 0 9990
2 00047 66.6657 311.1866 0214650 45.6793 316.1686 14.44725995397850
Epoch (UTC): | 15 June 2025 16:44:33 |
Eccentricity: | 0.0214650 |
inclination: | 66.6657° |
perigee height: | 590 km |
apogee height: | 896 km |
right ascension of ascending node: | 311.1866° |
argument of perigee: | 45.6793° |
revolutions per day: | 14.44725995 |
mean anomaly at epoch: | 316.1686° |
orbit number at epoch: | 39785 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|