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 24263.53100803 .00125736 00000-0 12424-2 0 9990
2 40911 97.4600 287.1643 0001172 308.5206 51.5948 15.65483876499231
| Epoch (UTC): | 19 September 2024 12:44:39 |
| Eccentricity: | 0.0001172 |
| inclination: | 97.4600° |
| perigee height: | 371 km |
| apogee height: | 372 km |
| right ascension of ascending node: | 287.1643° |
| argument of perigee: | 308.5206° |
| revolutions per day: | 15.65483876 |
| mean anomaly at epoch: | 51.5948° |
| orbit number at epoch: | 49923 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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