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 27949U 03043C 03322.30000000 -.00000045 +00000-0 +00000-0 0 9994
2 27949 006.8750 156.0810 6168022 202.5360 086.6250 01.75644504001063
| Epoch (UTC): | 18 November 2003 07:12:00 |
| Eccentricity: | 0.6168022 |
| inclination: | 6.8750° |
| perigee height: | 4741 km |
| apogee height: | 40535 km |
| right ascension of ascending node: | 156.0810° |
| argument of perigee: | 202.5360° |
| revolutions per day: | 1.75644504 |
| mean anomaly at epoch: | 86.6250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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