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 03544U 68103 A 69204.75818831 .02145351 +00000-0 +00000-0 0 9997
2 03544 051.5063 008.1656 0009291 001.9674 358.1291 16.44970317039634
| Epoch (UTC): | 23 July 1969 18:11:47 |
| Eccentricity: | 0.0009291 |
| inclination: | 51.5063° |
| perigee height: | 146 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 8.1656° |
| argument of perigee: | 1.9674° |
| revolutions per day: | 16.44970317 |
| mean anomaly at epoch: | 358.1291° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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