View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 36416U 10009D 24283.73703525 .00004007 00000-0 10002-2 0 9997
2 36416 63.3981 274.6730 0645011 359.4773 0.5518 13.71194100730125
Epoch (UTC): | 09 October 2024 17:41:19 |
Eccentricity: | 0.0645011 |
inclination: | 63.3981° |
perigee height: | 519 km |
apogee height: | 1471 km |
right ascension of ascending node: | 274.6730° |
argument of perigee: | 359.4773° |
revolutions per day: | 13.71194100 |
mean anomaly at epoch: | 0.5518° |
orbit number at epoch: | 73012 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|