View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 14064U 83044A 23151.88945864 .00002977 00000-0 22055-3 0 9990
2 14064 65.0003 19.3502 0108586 263.8735 95.0004 15.00558492 48484
Epoch (UTC): | 31 May 2023 21:20:49 |
Eccentricity: | 0.0108586 |
inclination: | 65.0003° |
perigee height: | 490 km |
apogee height: | 640 km |
right ascension of ascending node: | 19.3502° |
argument of perigee: | 263.8735° |
revolutions per day: | 15.00558492 |
mean anomaly at epoch: | 95.0004° |
orbit number at epoch: | 4848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|