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 07802U 75039 B 79043.84672902 .01220847 +00000-0 +00000-0 0 9996
2 07802 029.9263 089.4622 0075580 239.4754 131.2973 16.08854092202272
| Epoch (UTC): | 12 February 1979 20:19:17 |
| Eccentricity: | 0.0075580 |
| inclination: | 29.9263° |
| perigee height: | 200 km |
| apogee height: | 300 km |
| right ascension of ascending node: | 89.4622° |
| argument of perigee: | 239.4754° |
| revolutions per day: | 16.08854092 |
| mean anomaly at epoch: | 131.2973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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