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 04371U 70029 A 70101.81875742 .00099999 +00000-0 +00000-0 0 00013
2 04371 032.5642 350.1479 0010140 148.2777 356.5409 16.30346403000002
| Epoch (UTC): | 11 April 1970 19:39:00 |
| Eccentricity: | 0.0010140 |
| inclination: | 32.5642° |
| perigee height: | 185 km |
| apogee height: | 198 km |
| right ascension of ascending node: | 350.1479° |
| argument of perigee: | 148.2777° |
| revolutions per day: | 16.30346403 |
| mean anomaly at epoch: | 356.5409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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