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 06977U 73101 A 78344.43215764 .02836540 +88105-2 +35335-3 0 9993
2 06977 067.9426 343.9822 0001285 206.7624 153.1588 16.36031946276396
| Epoch (UTC): | 10 December 1978 10:22:18 |
| Eccentricity: | 0.0001285 |
| inclination: | 67.9426° |
| perigee height: | 175 km |
| apogee height: | 177 km |
| right ascension of ascending node: | 343.9822° |
| argument of perigee: | 206.7624° |
| revolutions per day: | 16.36031946 |
| mean anomaly at epoch: | 153.1588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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