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 40911U 15049N 23081.88223590 .00018250 00000-0 72561-3 0 9995
2 40911 97.4936 89.6770 0013829 99.5967 20.0613 15.25258460415190
| Epoch (UTC): | 22 March 2023 21:10:25 |
| Eccentricity: | 0.0013829 |
| inclination: | 97.4936° |
| perigee height: | 480 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 89.6770° |
| argument of perigee: | 99.5967° |
| revolutions per day: | 15.25258460 |
| mean anomaly at epoch: | 20.0613° |
| orbit number at epoch: | 41519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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