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 08450U 75110 A 75348.91805791 .00076525 +00000-0 +00000-0 0 9993
2 08450 062.8059 194.5624 0112575 106.9635 254.3835 15.93175436003064
| Epoch (UTC): | 14 December 1975 22:02:00 |
| Eccentricity: | 0.0112575 |
| inclination: | 62.8059° |
| perigee height: | 218 km |
| apogee height: | 368 km |
| right ascension of ascending node: | 194.5624° |
| argument of perigee: | 106.9635° |
| revolutions per day: | 15.93175436 |
| mean anomaly at epoch: | 254.3835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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