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 18281.91581316 0.00000000 00000-0 00000-0 0 06
2 33490 5.2615 31.3428 0005001 6.6779 353.2021 1.00270000 08
| Epoch (UTC): | 08 October 2018 21:58:46 |
| Eccentricity: | 0.0005001 |
| inclination: | 5.2615° |
| perigee height: | 35765 km |
| apogee height: | 35808 km |
| right ascension of ascending node: | 31.3428° |
| argument of perigee: | 6.6779° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 353.2021° |
| 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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