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 15755U 85042A 25350.29575928 -.00000061 00000-0 -60434-5 0 9995
2 15755 71.1122 301.8212 0037561 268.6486 91.0338 14.20962715101180
| Epoch (UTC): | 16 December 2025 07:05:53 |
| Eccentricity: | 0.0037561 |
| inclination: | 71.1122° |
| perigee height: | 795 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 301.8212° |
| argument of perigee: | 268.6486° |
| revolutions per day: | 14.20962715 |
| mean anomaly at epoch: | 91.0338° |
| orbit number at epoch: | 10118 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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