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 00034U 60005 A 62247.41570340 .02051518 +00000-0 +00000-0 0 01481
2 00034 064.9604 254.3998 0000000 066.3194 286.6963 16.39651632131532
| Epoch (UTC): | 04 September 1962 09:58:36 |
| Eccentricity: | 0.0000000 |
| inclination: | 64.9604° |
| perigee height: | 167 km |
| apogee height: | 167 km |
| right ascension of ascending node: | 254.3998° |
| argument of perigee: | 66.3194° |
| revolutions per day: | 16.39651632 |
| mean anomaly at epoch: | 286.6963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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