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 2768U 67040D 75042.57142285 -.00000859 00000-0 10000-3 0 9999
2 2768 35.1200 158.1261 7498300 182.8409 167.1313 0.50865911 13857
| Epoch (UTC): | 11 February 1975 13:42:50 |
| Eccentricity: | 0.7498300 |
| inclination: | 35.1200° |
| perigee height: | 10205 km |
| apogee height: | 109617 km |
| right ascension of ascending node: | 158.1261° |
| argument of perigee: | 182.8409° |
| revolutions per day: | 0.50865911 |
| mean anomaly at epoch: | 167.1313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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