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 00217U 61035 A 62224.81690329 .02183794 +00000-0 +00000-0 0 9993
2 00217 089.6614 069.6393 0000000 306.0785 209.0990 16.34065792036103
| Epoch (UTC): | 12 August 1962 19:36:20 |
| Eccentricity: | 0.0000000 |
| inclination: | 89.6614° |
| perigee height: | 181 km |
| apogee height: | 181 km |
| right ascension of ascending node: | 69.6393° |
| argument of perigee: | 306.0785° |
| revolutions per day: | 16.34065792 |
| mean anomaly at epoch: | 209.0990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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