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 02765U 67040A 71123.79930556 +.00000148 +00000-0 +00000-0 0 00270
2 02765 037.3528 131.5567 0700400 250.3854 299.6693 00.21525700003083
| Epoch (UTC): | 03 May 1971 19:11:00 |
| Eccentricity: | 0.0700400 |
| inclination: | 37.3528° |
| perigee height: | 102991 km |
| apogee height: | 119465 km |
| right ascension of ascending node: | 131.5567° |
| argument of perigee: | 250.3854° |
| revolutions per day: | 0.21525700 |
| mean anomaly at epoch: | 299.6693° |
| orbit number at epoch: | 308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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