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 27937U 03041A 18245.03285780 0.00000000 00000-0 00000-0 0 02
2 27937 10.1287 61.1102 0042905 216.2657 143.4531 1.00270000 00
| Epoch (UTC): | 02 September 2018 00:47:18 |
| Eccentricity: | 0.0042905 |
| inclination: | 10.1287° |
| perigee height: | 35606 km |
| apogee height: | 35967 km |
| right ascension of ascending node: | 61.1102° |
| argument of perigee: | 216.2657° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 143.4531° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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