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 18046.56418910 0.00000000 00000-0 00000-0 0 00
2 23223 11.2168 32.2277 0031108 144.9419 215.2786 1.00270000 02
| Epoch (UTC): | 15 February 2018 13:32:25 |
| Eccentricity: | 0.0031108 |
| inclination: | 11.2168° |
| perigee height: | 35655 km |
| apogee height: | 35918 km |
| right ascension of ascending node: | 32.2277° |
| argument of perigee: | 144.9419° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 215.2786° |
| 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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