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 40046U 14033AN 23273.06093989 .00006067 00000-0 77979-3 0 9997
2 40046 97.6547 91.3587 0053387 53.8294 306.7840 14.80497039499166
| Epoch (UTC): | 30 September 2023 01:27:45 |
| Eccentricity: | 0.0053387 |
| inclination: | 97.6547° |
| perigee height: | 590 km |
| apogee height: | 665 km |
| right ascension of ascending node: | 91.3587° |
| argument of perigee: | 53.8294° |
| revolutions per day: | 14.80497039 |
| mean anomaly at epoch: | 306.7840° |
| orbit number at epoch: | 49916 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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