View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 05492U 71083 B 78261.38305018 .02952915 +32368-1 +63252-3 0 08436
2 05492 033.0701 268.2001 0005010 235.2871 124.7198 16.33010571394262
| Epoch (UTC): | 18 September 1978 09:11:35 |
| Eccentricity: | 0.0005010 |
| inclination: | 33.0701° |
| perigee height: | 181 km |
| apogee height: | 188 km |
| right ascension of ascending node: | 268.2001° |
| argument of perigee: | 235.2871° |
| revolutions per day: | 16.33010571 |
| mean anomaly at epoch: | 124.7198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|