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 data is extracted from the following two-line orbital elements,
1 26061U 00004A 03303.41062303 .00002252 00000-0 75720-3 0 9734
2 26061 100.1904 47.3011 0034615 281.6926 78.0378 14.38082544197011
| Epoch (UTC): | 30 October 2003 09:51:17 |
| Eccentricity: | 0.0034615 |
| inclination: | 100.1904° |
| perigee height: | 740 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 47.3011° |
| argument of perigee: | 281.6926° |
| revolutions per day: | 14.38082544 |
| mean anomaly at epoch: | 78.0378° |
| orbit number at epoch: | 19701 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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