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 25889U 99044A 99349.53219064 .25057373 64258-5 38098-2 0 9994
2 25889 067.0869 182.7559 0038317 064.7636 342.3767 16.31332832 19072
| Epoch (UTC): | 15 December 1999 12:46:21 |
| Eccentricity: | 0.0038317 |
| inclination: | 67.0869° |
| perigee height: | 164 km |
| apogee height: | 214 km |
| right ascension of ascending node: | 182.7559° |
| argument of perigee: | 64.7636° |
| revolutions per day: | 16.31332832 |
| mean anomaly at epoch: | 342.3767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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