View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 06633U 73027 A 79185.88914720 .01109374 +00000-0 +00000-0 0 9991
2 06633 050.0279 012.4010 0004938 264.3626 095.7798 16.18386537348710
| Epoch (UTC): | 04 July 1979 21:20:22 |
| Eccentricity: | 0.0004938 |
| inclination: | 50.0279° |
| perigee height: | 220 km |
| apogee height: | 227 km |
| right ascension of ascending node: | 12.4010° |
| argument of perigee: | 264.3626° |
| revolutions per day: | 16.18386537 |
| mean anomaly at epoch: | 95.7798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|