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 00904U 64065 A 64286.36936185 .01500201 +00000-0 +00000-0 0 00014
2 00904 064.7172 168.8277 0119390 054.9930 306.1552 16.06260978000012
| Epoch (UTC): | 12 October 1964 08:51:52 |
| Eccentricity: | 0.0119390 |
| inclination: | 64.7172° |
| perigee height: | 178 km |
| apogee height: | 336 km |
| right ascension of ascending node: | 168.8277° |
| argument of perigee: | 54.9930° |
| revolutions per day: | 16.06260978 |
| mean anomaly at epoch: | 306.1552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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