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 26150.07109272 +.00000000 +00000-0 +12883-3 0 00006
2 05560 92.7005 178.0210 0016195 161.3807 198.7995 14.50836255 05
| Epoch (UTC): | 30 May 2026 01:42:22 |
| Eccentricity: | 0.0016195 |
| inclination: | 92.7005° |
| perigee height: | 711 km |
| apogee height: | 734 km |
| right ascension of ascending node: | 178.0210° |
| argument of perigee: | 161.3807° |
| revolutions per day: | 14.50836255 |
| mean anomaly at epoch: | 198.7995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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