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 42986U 17037E 25322.50133106 .00002312 00000-0 21019-3 0 9994
2 42986 97.5107 339.6288 0067186 215.8483 143.8220 14.94472906437480
| Epoch (UTC): | 18 November 2025 12:01:55 |
| Eccentricity: | 0.0067186 |
| inclination: | 97.5107° |
| perigee height: | 537 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 339.6288° |
| argument of perigee: | 215.8483° |
| revolutions per day: | 14.94472906 |
| mean anomaly at epoch: | 143.8220° |
| orbit number at epoch: | 43748 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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