View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13176U 82033 C 82189.74122157 .13436384 +56284-4 +84933-3 0 01107
2 13176 051.5694 093.2077 0010159 253.7964 106.2560 16.40895611012712
| Epoch (UTC): | 08 July 1982 17:47:21 |
| Eccentricity: | 0.0010159 |
| inclination: | 51.5694° |
| perigee height: | 157 km |
| apogee height: | 170 km |
| right ascension of ascending node: | 93.2077° |
| argument of perigee: | 253.7964° |
| revolutions per day: | 16.40895611 |
| mean anomaly at epoch: | 106.2560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|