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 00049U 60009 A 68144.86617407 .41988289 +00000-0 +00000-0 0 9999
2 00049 047.1857 303.1560 0018299 276.1888 083.6866 15.53427992360298
| Epoch (UTC): | 23 May 1968 20:47:17 |
| Eccentricity: | 0.0018299 |
| inclination: | 47.1857° |
| perigee height: | 394 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 303.1560° |
| argument of perigee: | 276.1888° |
| revolutions per day: | 15.53427992 |
| mean anomaly at epoch: | 83.6866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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