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 41783U 16059A 25013.03311585 .00001282 00000-0 24106-3 0 9990
2 41783 97.8279 28.5514 0033374 74.9629 285.5265 14.65893269443275
| Epoch (UTC): | 13 January 2025 00:47:41 |
| Eccentricity: | 0.0033374 |
| inclination: | 97.8279° |
| perigee height: | 650 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 28.5514° |
| argument of perigee: | 74.9629° |
| revolutions per day: | 14.65893269 |
| mean anomaly at epoch: | 285.5265° |
| orbit number at epoch: | 44327 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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