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 18380U 87083 A 87285.83916663 .00286812 +87302-5 +39762-3 0 00249
2 18380 062.8211 098.7516 0115800 113.5296 248.8099 15.93803561002126
| Epoch (UTC): | 12 October 1987 20:08:23 |
| Eccentricity: | 0.0115800 |
| inclination: | 62.8211° |
| perigee height: | 214 km |
| apogee height: | 369 km |
| right ascension of ascending node: | 98.7516° |
| argument of perigee: | 113.5296° |
| revolutions per day: | 15.93803561 |
| mean anomaly at epoch: | 248.8099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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