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 40912U 15049P 23092.24695914 .00049093 00000-0 13063-2 0 9991
2 40912 97.4251 108.8281 0009605 12.1292 49.2409 15.38013454417915
| Epoch (UTC): | 02 April 2023 05:55:37 |
| Eccentricity: | 0.0009605 |
| inclination: | 97.4251° |
| perigee height: | 445 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 108.8281° |
| argument of perigee: | 12.1292° |
| revolutions per day: | 15.38013454 |
| mean anomaly at epoch: | 49.2409° |
| orbit number at epoch: | 41791 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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