View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 06142U 72061 A 79306.11161986 .12447094 +38058-5 +70923-2 0 00890
2 06142 037.6650 352.5192 0009051 287.8712 072.0909 16.17916814392521
| Epoch (UTC): | 02 November 1979 02:40:43 |
| Eccentricity: | 0.0009051 |
| inclination: | 37.6650° |
| perigee height: | 219 km |
| apogee height: | 231 km |
| right ascension of ascending node: | 352.5192° |
| argument of perigee: | 287.8712° |
| revolutions per day: | 16.17916814 |
| mean anomaly at epoch: | 72.0909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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