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 01085U 65009 A 78260.10482279 .18241631 +00000-0 +00000-0 0 02247
2 01085 031.7228 272.6338 0025530 308.3466 054.6075 16.42422799752002
| Epoch (UTC): | 17 September 1978 02:30:56 |
| Eccentricity: | 0.0025530 |
| inclination: | 31.7228° |
| perigee height: | 143 km |
| apogee height: | 176 km |
| right ascension of ascending node: | 272.6338° |
| argument of perigee: | 308.3466° |
| revolutions per day: | 16.42422799 |
| mean anomaly at epoch: | 54.6075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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