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 24744U 97010A 99298.01559523 +.18186949 +26149-5 +42558-3 0 9995
2 24744 097.1873 210.1564 0006828 227.8300 267.4377 16.46029259148792
| Epoch (UTC): | 25 October 1999 00:22:27 |
| Eccentricity: | 0.0006828 |
| inclination: | 97.1873° |
| perigee height: | 145 km |
| apogee height: | 154 km |
| right ascension of ascending node: | 210.1564° |
| argument of perigee: | 227.8300° |
| revolutions per day: | 16.46029259 |
| mean anomaly at epoch: | 267.4377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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