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 26598U 95008AA 00303.73191600 .99999999 74234-5 18168-2 0 9998
2 26598 065.8165 222.8288 0022462 324.0548 036.2378 16.49989909 33
| Epoch (UTC): | 29 October 2000 17:33:57 |
| Eccentricity: | 0.0022462 |
| inclination: | 65.8165° |
| perigee height: | 125 km |
| apogee height: | 154 km |
| right ascension of ascending node: | 222.8288° |
| argument of perigee: | 324.0548° |
| revolutions per day: | 16.49989909 |
| mean anomaly at epoch: | 36.2378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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