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 11536U 79083 A 79287.00206205 .00173790 +00000-0 +01765-5 0 9992
2 11536 062.8069 115.0675 0100841 115.1822 246.0892 15.98830795002927
| Epoch (UTC): | 14 October 1979 00:02:58 |
| Eccentricity: | 0.0100841 |
| inclination: | 62.8069° |
| perigee height: | 210 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 115.0675° |
| argument of perigee: | 115.1822° |
| revolutions per day: | 15.98830795 |
| mean anomaly at epoch: | 246.0892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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