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 04409U 70042 A 70168.32234452 .00267965 +00000-0 +00000-0 0 00061
2 04409 051.7409 013.6339 0055676 048.0199 312.5500 16.15811055001123
| Epoch (UTC): | 17 June 1970 07:44:10 |
| Eccentricity: | 0.0055676 |
| inclination: | 51.7409° |
| perigee height: | 194 km |
| apogee height: | 268 km |
| right ascension of ascending node: | 13.6339° |
| argument of perigee: | 48.0199° |
| revolutions per day: | 16.15811055 |
| mean anomaly at epoch: | 312.5500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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