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 25744U 99028A 05334.15210437 0.00000000 00000-0 00000-0 0 01
2 25744 63.4412 124.9814 0242000 294.1240 65.8760 9.69817792 03
| Epoch (UTC): | 30 November 2005 03:39:01 |
| Eccentricity: | 0.0242000 |
| inclination: | 63.4412° |
| perigee height: | 2685 km |
| apogee height: | 3135 km |
| right ascension of ascending node: | 124.9814° |
| argument of perigee: | 294.1240° |
| revolutions per day: | 9.69817792 |
| mean anomaly at epoch: | 65.8760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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