View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 24278U 96046B 23088.48040238 .00000044 00000-0 83760-4 0 9994
2 24278 98.5234 77.9182 0349185 263.6536 92.4735 13.53139903314152
Epoch (UTC): | 29 March 2023 11:31:46 |
Eccentricity: | 0.0349185 |
inclination: | 98.5234° |
perigee height: | 801 km |
apogee height: | 1320 km |
right ascension of ascending node: | 77.9182° |
argument of perigee: | 263.6536° |
revolutions per day: | 13.53139903 |
mean anomaly at epoch: | 92.4735° |
orbit number at epoch: | 31415 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|