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 15993U 85076B 25346.93705458 -.00000341 00000-0 00000-0 0 9993
2 15993 13.4520 340.1827 0003586 322.9006 236.3294 0.99763171117734
| Epoch (UTC): | 12 December 2025 22:29:21 |
| Eccentricity: | 0.0003586 |
| inclination: | 13.4520° |
| perigee height: | 35914 km |
| apogee height: | 35944 km |
| right ascension of ascending node: | 340.1827° |
| argument of perigee: | 322.9006° |
| revolutions per day: | 0.99763171 |
| mean anomaly at epoch: | 236.3294° |
| orbit number at epoch: | 11773 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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