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 26704U 01007C 01061.30049187 +.51784825 +00000-0 +11655-0 0 9995
2 26704 097.7809 072.0042 0042957 201.7198 158.6845 15.86499875001506
| Epoch (UTC): | 02 March 2001 07:12:42 |
| Eccentricity: | 0.0042957 |
| inclination: | 97.7809° |
| perigee height: | 283 km |
| apogee height: | 341 km |
| right ascension of ascending node: | 72.0042° |
| argument of perigee: | 201.7198° |
| revolutions per day: | 15.86499875 |
| mean anomaly at epoch: | 158.6845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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