View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28773U 05025A 23027.07824620 .00013504 00000-0 53168-3 0 9991
2 28773 31.3797 276.9355 0003290 120.4003 239.6971 15.24408166969132
Epoch (UTC): | 27 January 2023 01:52:40 |
Eccentricity: | 0.0003290 |
inclination: | 31.3797° |
perigee height: | 490 km |
apogee height: | 495 km |
right ascension of ascending node: | 276.9355° |
argument of perigee: | 120.4003° |
revolutions per day: | 15.24408166 |
mean anomaly at epoch: | 239.6971° |
orbit number at epoch: | 96913 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|