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 01274U 65022 A 65077.66520713 .00121346 +28604-4 +00000-0 0 00020
2 01274 064.7930 314.8909 0227292 070.5013 291.9522 15.83634739000064
| Epoch (UTC): | 18 March 1965 15:57:53 |
| Eccentricity: | 0.0227292 |
| inclination: | 64.7930° |
| perigee height: | 168 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 314.8909° |
| argument of perigee: | 70.5013° |
| revolutions per day: | 15.83634739 |
| mean anomaly at epoch: | 291.9522° |
| orbit number at epoch: | 6 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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