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 03534U 68100 B 79262.01512950 .18317528 -10952-4 +24864-3 0 9993
2 03534 032.8214 155.0214 0011423 314.3530 045.6474 16.42601773599050
| Epoch (UTC): | 19 September 1979 00:21:47 |
| Eccentricity: | 0.0011423 |
| inclination: | 32.8214° |
| perigee height: | 151 km |
| apogee height: | 166 km |
| right ascension of ascending node: | 155.0214° |
| argument of perigee: | 314.3530° |
| revolutions per day: | 16.42601773 |
| mean anomaly at epoch: | 45.6474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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