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 25424U 97074E 01058.79120260 .00007950 00000-0 45452-3 0 9999
2 25424 034.9670 285.9104 0001391 294.2847 065.8215 15.11784129141492
| Epoch (UTC): | 27 February 2001 18:59:19 |
| Eccentricity: | 0.0001391 |
| inclination: | 34.9670° |
| perigee height: | 530 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 285.9104° |
| argument of perigee: | 294.2847° |
| revolutions per day: | 15.11784129 |
| mean anomaly at epoch: | 65.8215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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