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 data is extracted from the following two-line orbital elements,
1 00091U 61008 A 61068.32560921 .00000000 +00000-0 +00000-0 0 00018
2 00091 064.9300 300.5999 0070000 095.0000 265.4066 16.39468422000015
| Epoch (UTC): | 09 March 1961 07:48:52 |
| Eccentricity: | 0.0070000 |
| inclination: | 64.9300° |
| perigee height: | 121 km |
| apogee height: | 213 km |
| right ascension of ascending node: | 300.5999° |
| argument of perigee: | 95.0000° |
| revolutions per day: | 16.39468422 |
| mean anomaly at epoch: | 265.4066° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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