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 06913U 73083 A 73323.94212164 .00061946 +06239-6 +00000-0 0 9999
2 06913 062.7999 192.1415 0130338 113.7984 247.6840 15.91198635003054
| Epoch (UTC): | 19 November 1973 22:36:39 |
| Eccentricity: | 0.0130338 |
| inclination: | 62.7999° |
| perigee height: | 212 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 192.1415° |
| argument of perigee: | 113.7984° |
| revolutions per day: | 15.91198635 |
| mean anomaly at epoch: | 247.6840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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