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 20580U 90037B 15059.59054332 .00002863 00000-0 17553-3 0 9998
2 20580 028.4699 149.9813 0003260 145.0129 357.1098 15.06898039163410
| Epoch (UTC): | 28 February 2015 14:10:22 |
| Eccentricity: | 0.0003260 |
| inclination: | 28.4699° |
| perigee height: | 543 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 149.9813° |
| argument of perigee: | 145.0129° |
| revolutions per day: | 15.06898039 |
| mean anomaly at epoch: | 357.1098° |
| orbit number at epoch: | 16341 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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