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 16271.84052083 .00001006 00000-0 51633-4 0 9990
2 20580 28.4702 300.7545 0002571 228.7088 144.8375 15.08513420250620
| Epoch (UTC): | 27 September 2016 20:10:21 |
| Eccentricity: | 0.0002571 |
| inclination: | 28.4702° |
| perigee height: | 539 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 300.7545° |
| argument of perigee: | 228.7088° |
| revolutions per day: | 15.08513420 |
| mean anomaly at epoch: | 144.8375° |
| orbit number at epoch: | 25062 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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