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 23223U 94054A 18276.92681626 0.00000000 00000-0 00000-0 0 01
2 23223 11.4167 30.2042 0033622 151.7369 208.4609 1.00270000 02
| Epoch (UTC): | 03 October 2018 22:14:36 |
| Eccentricity: | 0.0033622 |
| inclination: | 11.4167° |
| perigee height: | 35645 km |
| apogee height: | 35928 km |
| right ascension of ascending node: | 30.2042° |
| argument of perigee: | 151.7369° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 208.4609° |
| 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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