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 40910U 15049M 23332.56721317 .00087900 00000-0 13421-2 0 9995
2 40910 97.4478 349.9625 0003907 232.7988 127.2909 15.54122701454383
| Epoch (UTC): | 28 November 2023 13:36:47 |
| Eccentricity: | 0.0003907 |
| inclination: | 97.4478° |
| perigee height: | 402 km |
| apogee height: | 407 km |
| right ascension of ascending node: | 349.9625° |
| argument of perigee: | 232.7988° |
| revolutions per day: | 15.54122701 |
| mean anomaly at epoch: | 127.2909° |
| orbit number at epoch: | 45438 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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