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 00504U 62067 B 68237.98186891 .06182616 +00000-0 +00000-0 0 9996
2 00504 070.2141 090.6538 0018907 043.7589 316.5020 16.37295104277728
| Epoch (UTC): | 24 August 1968 23:33:53 |
| Eccentricity: | 0.0018907 |
| inclination: | 70.2141° |
| perigee height: | 160 km |
| apogee height: | 185 km |
| right ascension of ascending node: | 90.6538° |
| argument of perigee: | 43.7589° |
| revolutions per day: | 16.37295104 |
| mean anomaly at epoch: | 316.5020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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