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 42849U 17042AA 23271.51629308 .00003879 00000-0 35165-3 0 9990
2 42849 97.3793 108.2681 0006225 212.0028 148.0817 14.95863620338213
| Epoch (UTC): | 28 September 2023 12:23:27 |
| Eccentricity: | 0.0006225 |
| inclination: | 97.3793° |
| perigee height: | 575 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 108.2681° |
| argument of perigee: | 212.0028° |
| revolutions per day: | 14.95863620 |
| mean anomaly at epoch: | 148.0817° |
| orbit number at epoch: | 33821 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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