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 23855U 96026A 18046.45659606 0.00000000 00000-0 00000-0 0 09
2 23855 9.4496 359.3377 0407580 252.9462 102.6290 1.00270000 08
| Epoch (UTC): | 15 February 2018 10:57:29 |
| Eccentricity: | 0.0407580 |
| inclination: | 9.4496° |
| perigee height: | 34068 km |
| apogee height: | 37505 km |
| right ascension of ascending node: | 359.3377° |
| argument of perigee: | 252.9462° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 102.6290° |
| 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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