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 data is extracted from the following two-line orbital elements,
1 02766U 67040B 74251.73833333 -.00000154 +00000-0 +00000-0 0 00486
2 02766 037.1690 130.8800 1052100 072.5800 207.4990 00.21464491005670
| Epoch (UTC): | 08 September 1974 17:43:12 |
| Eccentricity: | 0.1052100 |
| inclination: | 37.1690° |
| perigee height: | 99055 km |
| apogee height: | 123848 km |
| right ascension of ascending node: | 130.8800° |
| argument of perigee: | 72.5800° |
| revolutions per day: | 0.21464491 |
| mean anomaly at epoch: | 207.4990° |
| orbit number at epoch: | 567 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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