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 40028U 14033U 19345.82250035 +.00000293 +00000-0 +37251-4 0 9998
2 40028 097.9141 265.8454 0013115 194.3994 165.6856 14.88867840297516
| Epoch (UTC): | 11 December 2019 19:44:24 |
| Eccentricity: | 0.0013115 |
| inclination: | 97.9141° |
| perigee height: | 592 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 265.8454° |
| argument of perigee: | 194.3994° |
| revolutions per day: | 14.88867840 |
| mean anomaly at epoch: | 165.6856° |
| orbit number at epoch: | 29751 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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