View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27607U 02058C 22181.66763004 .00000178 00000-0 45038-4 0 9993
2 27607 64.5547 261.4640 0079113 291.8890 67.3814 14.76146894 50325
| Epoch (UTC): | 30 June 2022 16:01:23 |
| Eccentricity: | 0.0079113 |
| inclination: | 64.5547° |
| perigee height: | 586 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 261.4640° |
| argument of perigee: | 291.8890° |
| revolutions per day: | 14.76146894 |
| mean anomaly at epoch: | 67.3814° |
| orbit number at epoch: | 5032 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|