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 49317U 21091C 24358.20158920 .00039568 00000-0 10154-2 0 9990
2 49317 97.4285 191.4328 0010454 127.9538 232.2654 15.39170576177483
| Epoch (UTC): | 23 December 2024 04:50:17 |
| Eccentricity: | 0.0010454 |
| inclination: | 97.4285° |
| perigee height: | 441 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 191.4328° |
| argument of perigee: | 127.9538° |
| revolutions per day: | 15.39170576 |
| mean anomaly at epoch: | 232.2654° |
| orbit number at epoch: | 17748 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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