View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00091U 61008 A 61068.32560921 .00000000 +00000-0 +00000-0 0 00018
2 00091 064.9300 300.5999 0070000 095.0000 265.4066 16.39468422000015
| Epoch (UTC): | 09 March 1961 07:48:52 |
| Eccentricity: | 0.0070000 |
| inclination: | 64.9300° |
| perigee height: | 121 km |
| apogee height: | 213 km |
| right ascension of ascending node: | 300.5999° |
| argument of perigee: | 95.0000° |
| revolutions per day: | 16.39468422 |
| mean anomaly at epoch: | 265.4066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|