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 43162U 26145.62092611 +.00000000 +00000-0 +00000-0 0 00004
2 43162 2.1694 11.0668 0002214 44.1839 252.0832 1.00272235 04
| Epoch (UTC): | 25 May 2026 14:54:08 |
| Eccentricity: | 0.0002214 |
| inclination: | 2.1694° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 11.0668° |
| argument of perigee: | 44.1839° |
| revolutions per day: | 1.00272235 |
| mean anomaly at epoch: | 252.0832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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