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 03141U 68017 A 90320.77793654 .19017804 +52283-4 +41034-3 0 02591
2 03141 059.3209 173.6220 0005157 233.8627 126.3237 16.46470904233417
| Epoch (UTC): | 16 November 1990 18:40:13 |
| Eccentricity: | 0.0005157 |
| inclination: | 59.3209° |
| perigee height: | 145 km |
| apogee height: | 152 km |
| right ascension of ascending node: | 173.6220° |
| argument of perigee: | 233.8627° |
| revolutions per day: | 16.46470904 |
| mean anomaly at epoch: | 126.3237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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