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 33490U 09001A 18125.34260844 0.00000000 00000-0 00000-0 0 00
2 33490 5.1404 30.5668 0010678 324.2638 35.6674 1.00270000 04
| Epoch (UTC): | 05 May 2018 08:13:21 |
| Eccentricity: | 0.0010678 |
| inclination: | 5.1404° |
| perigee height: | 35741 km |
| apogee height: | 35832 km |
| right ascension of ascending node: | 30.5668° |
| argument of perigee: | 324.2638° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 35.6674° |
| 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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