View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25682U 99020A 23030.58073356 .00000641 00000-0 14309-3 0 9999
2 25682 97.9503 74.7184 0001646 90.5866 269.5504 14.59905371265705
Epoch (UTC): | 30 January 2023 13:56:15 |
Eccentricity: | 0.0001646 |
inclination: | 97.9503° |
perigee height: | 692 km |
apogee height: | 694 km |
right ascension of ascending node: | 74.7184° |
argument of perigee: | 90.5866° |
revolutions per day: | 14.59905371 |
mean anomaly at epoch: | 269.5504° |
orbit number at epoch: | 26570 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|