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 07427U 74070 A 77164.43856214 .05755034 +00000-0 +00000-0 0 06958
2 07427 097.9353 227.2513 0014208 347.8335 015.1564 16.35793144153136
| Epoch (UTC): | 13 June 1977 10:31:31 |
| Eccentricity: | 0.0014208 |
| inclination: | 97.9353° |
| perigee height: | 168 km |
| apogee height: | 186 km |
| right ascension of ascending node: | 227.2513° |
| argument of perigee: | 347.8335° |
| revolutions per day: | 16.35793144 |
| mean anomaly at epoch: | 15.1564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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