View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 05675U 71109 A 78344.07105664 .03693295 +00000-0 +17952-2 0 9999
2 05675 082.9509 212.0114 0005439 118.3447 242.4586 16.16119143390105
| Epoch (UTC): | 10 December 1978 01:42:19 |
| Eccentricity: | 0.0005439 |
| inclination: | 82.9509° |
| perigee height: | 226 km |
| apogee height: | 234 km |
| right ascension of ascending node: | 212.0114° |
| argument of perigee: | 118.3447° |
| revolutions per day: | 16.16119143 |
| mean anomaly at epoch: | 242.4586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|