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 20325.68554119 0.00000000 00000-0 00000-0 0 00
2 23855 8.9700 354.7433 0379130 271.1616 88.8384 1.00270000 04
| Epoch (UTC): | 20 November 2020 16:27:10 |
| Eccentricity: | 0.0379130 |
| inclination: | 8.9700° |
| perigee height: | 34188 km |
| apogee height: | 37385 km |
| right ascension of ascending node: | 354.7433° |
| argument of perigee: | 271.1616° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 88.8384° |
| 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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