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 19236U 81065 D 90105.54873724 .10230099 +18000-5 +73484-2 06483
2 19236 097.7289 113.0824 0009944 212.0183 151.0430 16.15822100103146
| Epoch (UTC): | 15 April 1990 13:10:10 |
| Eccentricity: | 0.0009944 |
| inclination: | 97.7289° |
| perigee height: | 224 km |
| apogee height: | 237 km |
| right ascension of ascending node: | 113.0824° |
| argument of perigee: | 212.0183° |
| revolutions per day: | 16.15822100 |
| mean anomaly at epoch: | 151.0430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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