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 07591U 74104 A 77033.21536148 .01513000 +00000-0 +00000-0 0 9998
2 07591 051.5688 125.4116 0000792 346.2799 013.7217 16.32332898121779
| Epoch (UTC): | 02 February 1977 05:10:07 |
| Eccentricity: | 0.0000792 |
| inclination: | 51.5688° |
| perigee height: | 186 km |
| apogee height: | 187 km |
| right ascension of ascending node: | 125.4116° |
| argument of perigee: | 346.2799° |
| revolutions per day: | 16.32332898 |
| mean anomaly at epoch: | 13.7217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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