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 03595U 68109 A 70339.19222221 .00000000 +00000-0 +00000-0 0 9999
2 03595 061.7822 104.4787 7665399 317.6551 011.1605 00.21477763008957
| Epoch (UTC): | 05 December 1970 04:36:47 |
| Eccentricity: | 0.7665399 |
| inclination: | 61.7822° |
| perigee height: | 21119 km |
| apogee height: | 201684 km |
| right ascension of ascending node: | 104.4787° |
| argument of perigee: | 317.6551° |
| revolutions per day: | 0.21477763 |
| mean anomaly at epoch: | 11.1605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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