View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00595U 63023 A 63169.77883834 .00945882 +00000-0 +00000-0 0 00049
2 00595 064.9184 073.1054 0021863 078.4674 281.7784 16.35626644000391
| Epoch (UTC): | 18 June 1963 18:41:31 |
| Eccentricity: | 0.0021863 |
| inclination: | 64.9184° |
| perigee height: | 163 km |
| apogee height: | 192 km |
| right ascension of ascending node: | 73.1054° |
| argument of perigee: | 78.4674° |
| revolutions per day: | 16.35626644 |
| mean anomaly at epoch: | 281.7784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|