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 40128U 14050A 23331.96505903 -.00000099 00000-0 00000-0 0 9993
2 40128 49.8586 311.1796 1606240 143.5671 228.5386 1.85519573 61028
| Epoch (UTC): | 27 November 2023 23:09:41 |
| Eccentricity: | 0.1606240 |
| inclination: | 49.8586° |
| perigee height: | 17105 km |
| apogee height: | 26093 km |
| right ascension of ascending node: | 311.1796° |
| argument of perigee: | 143.5671° |
| revolutions per day: | 1.85519573 |
| mean anomaly at epoch: | 228.5386° |
| orbit number at epoch: | 6102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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