View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 82U 61004B 23337.75915869 .00000650 00000-0 60213-3 0 9995
2 82 38.8497 197.2312 1163975 65.4494 306.2975 12.26439651962996
Epoch (UTC): | 03 December 2023 18:13:11 |
Eccentricity: | 0.1163975 |
inclination: | 38.8497° |
perigee height: | 640 km |
apogee height: | 2489 km |
right ascension of ascending node: | 197.2312° |
argument of perigee: | 65.4494° |
revolutions per day: | 12.26439651 |
mean anomaly at epoch: | 306.2975° |
orbit number at epoch: | 96299 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|