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 05560U 26160.07178794 +.00000000 +00000-0 +95710-4 0 00003
2 05560 92.6999 181.2421 0017336 130.2632 230.0094 14.50845046 03
| Epoch (UTC): | 09 June 2026 01:43:22 |
| Eccentricity: | 0.0017336 |
| inclination: | 92.6999° |
| perigee height: | 711 km |
| apogee height: | 735 km |
| right ascension of ascending node: | 181.2421° |
| argument of perigee: | 130.2632° |
| revolutions per day: | 14.50845046 |
| mean anomaly at epoch: | 230.0094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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