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 54160U 26145.29464275 +.00000000 +00000-0 -19360-4 0 00000
2 54160 53.2133 345.1936 0001237 132.1696 227.9402 15.08836719 01
| Epoch (UTC): | 25 May 2026 07:04:17 |
| Eccentricity: | 0.0001237 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 345.1936° |
| argument of perigee: | 132.1696° |
| revolutions per day: | 15.08836719 |
| mean anomaly at epoch: | 227.9402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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