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 is defined by the following mean orbital elements,
1 15595U 26022.25911750 +.00000000 +00000-0 +22363-3 0 00009
2 15595 108.0435 137.7238 0002377 273.2069 86.8802 14.39869192 01
| Epoch (UTC): | 22 January 2026 06:13:07 |
| Eccentricity: | 0.0002377 |
| inclination: | 108.0435° |
| perigee height: | 757 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 137.7238° |
| argument of perigee: | 273.2069° |
| revolutions per day: | 14.39869192 |
| mean anomaly at epoch: | 86.8802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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