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 24904U 97043B 13142.44368241 .00000225 00000-0 73316-4 0 3701
2 24904 086.3968 156.9021 0002383 106.6088 253.5369 14.34216110824729
| Epoch (UTC): | 22 May 2013 10:38:54 |
| Eccentricity: | 0.0002383 |
| inclination: | 86.3968° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 156.9021° |
| argument of perigee: | 106.6088° |
| revolutions per day: | 14.34216110 |
| mean anomaly at epoch: | 253.5369° |
| orbit number at epoch: | 82472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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