View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 04065U 69068 A 81065.97247172 .04669629 -10284-4 +89105-4 0 05718
2 04065 032.9448 124.8800 0001853 046.8850 313.2804 16.38245563647201
| Epoch (UTC): | 06 March 1981 23:20:21 |
| Eccentricity: | 0.0001853 |
| inclination: | 32.9448° |
| perigee height: | 169 km |
| apogee height: | 172 km |
| right ascension of ascending node: | 124.8800° |
| argument of perigee: | 46.8850° |
| revolutions per day: | 16.38245563 |
| mean anomaly at epoch: | 313.2804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|