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 00081U 61004 A 64099.25942492 .10394656 +00000-0 +00000-0 0 9999
2 00081 038.8448 136.7337 0200872 038.1868 323.2614 15.48210031142271
| Epoch (UTC): | 08 April 1964 06:13:34 |
| Eccentricity: | 0.0200872 |
| inclination: | 38.8448° |
| perigee height: | 285 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 136.7337° |
| argument of perigee: | 38.1868° |
| revolutions per day: | 15.48210031 |
| mean anomaly at epoch: | 323.2614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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