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 40906U 15049H 24279.50226076 .00103080 00000-0 15439-2 0 9996
2 40906 97.4692 299.9679 0003909 240.7479 119.3384 15.54595550501530
| Epoch (UTC): | 05 October 2024 12:03:15 |
| Eccentricity: | 0.0003909 |
| inclination: | 97.4692° |
| perigee height: | 400 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 299.9679° |
| argument of perigee: | 240.7479° |
| revolutions per day: | 15.54595550 |
| mean anomaly at epoch: | 119.3384° |
| orbit number at epoch: | 50153 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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