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 01381U 65039 A 79307.49303108 .09516714 -14427-4 +26558-3 0 03764
2 01381 031.7474 161.1695 0002959 273.9325 086.1002 16.32717544794788
| Epoch (UTC): | 03 November 1979 11:49:57 |
| Eccentricity: | 0.0002959 |
| inclination: | 31.7474° |
| perigee height: | 183 km |
| apogee height: | 187 km |
| right ascension of ascending node: | 161.1695° |
| argument of perigee: | 273.9325° |
| revolutions per day: | 16.32717544 |
| mean anomaly at epoch: | 86.1002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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