View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 32378U 07060A 22263.41779251 0.00001092 00000-0 00000-0 0 02
2 32378 63.4093 295.1602 7334324 272.3303 87.6697 2.00618642 03
Epoch (UTC): | 20 September 2022 10:01:37 |
Eccentricity: | 0.7334324 |
inclination: | 63.4093° |
perigee height: | 700 km |
apogee height: | 39653 km |
right ascension of ascending node: | 295.1602° |
argument of perigee: | 272.3303° |
revolutions per day: | 2.00618642 |
mean anomaly at epoch: | 87.6697° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|