View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 04791U 70105 A 70351.35049087 .00168070 +00000-0 +00000-0 0 9998
2 04791 072.8888 233.4277 0058690 044.5499 316.0382 16.12072372001112
| Epoch (UTC): | 17 December 1970 08:24:42 |
| Eccentricity: | 0.0058690 |
| inclination: | 72.8888° |
| perigee height: | 202 km |
| apogee height: | 280 km |
| right ascension of ascending node: | 233.4277° |
| argument of perigee: | 44.5499° |
| revolutions per day: | 16.12072372 |
| mean anomaly at epoch: | 316.0382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|