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 12554U 67092 E 89251.07962063 .00403496 +00000-0 +62774-1 0 9992
2 12554 089.1953 290.5862 0005365 232.1809 134.1507 14.73083904018199
| Epoch (UTC): | 08 September 1989 01:54:39 |
| Eccentricity: | 0.0005365 |
| inclination: | 89.1953° |
| perigee height: | 647 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 290.5862° |
| argument of perigee: | 232.1809° |
| revolutions per day: | 14.73083904 |
| mean anomaly at epoch: | 134.1507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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