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 40395U 95015G 23332.60490419 .00003413 00000-0 14634-2 0 9998
2 40395 98.6624 350.5534 0027801 116.9889 243.4134 14.25242955454736
| Epoch (UTC): | 28 November 2023 14:31:03 |
| Eccentricity: | 0.0027801 |
| inclination: | 98.6624° |
| perigee height: | 788 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 350.5534° |
| argument of perigee: | 116.9889° |
| revolutions per day: | 14.25242955 |
| mean anomaly at epoch: | 243.4134° |
| orbit number at epoch: | 45473 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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