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 15495U 85009B 15024.31463556 .00000243 00000-0 26664-4 0 01
2 15495 082.5255 286.7874 0019361 339.9248 020.1203 14.83439960620242
| Epoch (UTC): | 24 January 2015 07:33:04 |
| Eccentricity: | 0.0019361 |
| inclination: | 82.5255° |
| perigee height: | 605 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 286.7874° |
| argument of perigee: | 339.9248° |
| revolutions per day: | 14.83439960 |
| mean anomaly at epoch: | 20.1203° |
| orbit number at epoch: | 62024 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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