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 55160U 26145.31831286 +.00000000 +00000-0 +65323-4 0 00003
2 55160 87.9161 10.3945 0002232 80.4298 279.7086 13.17649633 05
| Epoch (UTC): | 25 May 2026 07:38:22 |
| Eccentricity: | 0.0002232 |
| inclination: | 87.9161° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3945° |
| argument of perigee: | 80.4298° |
| revolutions per day: | 13.17649633 |
| mean anomaly at epoch: | 279.7086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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