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 43254U 26145.42897429 +.00000000 +00000-0 +38122-4 0 00004
2 43254 86.3939 299.9367 0002060 90.7870 269.3562 14.34217987 01
| Epoch (UTC): | 25 May 2026 10:17:43 |
| Eccentricity: | 0.0002060 |
| inclination: | 86.3939° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 299.9367° |
| argument of perigee: | 90.7870° |
| revolutions per day: | 14.34217987 |
| mean anomaly at epoch: | 269.3562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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