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 07004U 73107B 13142.85963559 .00024333 00000-0 78165-3 0 3089
2 07004 073.9553 299.8761 0350787 180.5903 328.4169 14.89056802 12035
| Epoch (UTC): | 22 May 2013 20:37:52 |
| Eccentricity: | 0.0350787 |
| inclination: | 73.9553° |
| perigee height: | 356 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 299.8761° |
| argument of perigee: | 180.5903° |
| revolutions per day: | 14.89056802 |
| mean anomaly at epoch: | 328.4169° |
| orbit number at epoch: | 1203 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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