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 25860U 99039A 23151.69879809 .00000725 00000-0 10902-3 0 9998
2 25860 98.0897 198.6980 0001585 74.0540 286.0845 14.77502414284668
| Epoch (UTC): | 31 May 2023 16:46:16 |
| Eccentricity: | 0.0001585 |
| inclination: | 98.0897° |
| perigee height: | 636 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 198.6980° |
| argument of perigee: | 74.0540° |
| revolutions per day: | 14.77502414 |
| mean anomaly at epoch: | 286.0845° |
| orbit number at epoch: | 28466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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