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 23567U 95022A 18213.88372073 0.00000000 00000-0 00000-0 0 07
2 23567 14.2876 34.7000 0059523 93.3609 267.3386 1.00270000 06
| Epoch (UTC): | 01 August 2018 21:12:33 |
| Eccentricity: | 0.0059523 |
| inclination: | 14.2876° |
| perigee height: | 35536 km |
| apogee height: | 36037 km |
| right ascension of ascending node: | 34.7000° |
| argument of perigee: | 93.3609° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 267.3386° |
| 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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