View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 37855U 11061F 22221.68141749 .00008413 00000-0 36513-3 0 9993
2 37855 101.7152 8.9756 0151498 262.7346 95.6628 15.13037835589284
Epoch (UTC): | 09 August 2022 16:21:14 |
Eccentricity: | 0.0151498 |
inclination: | 101.7152° |
perigee height: | 422 km |
apogee height: | 631 km |
right ascension of ascending node: | 8.9756° |
argument of perigee: | 262.7346° |
revolutions per day: | 15.13037835 |
mean anomaly at epoch: | 95.6628° |
orbit number at epoch: | 58928 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|