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 43249U 26145.41628853 +.00000000 +00000-0 +67209-4 0 00008
2 43249 86.3939 299.9249 0002058 90.6049 269.5383 14.34218249 03
| Epoch (UTC): | 25 May 2026 09:59:27 |
| Eccentricity: | 0.0002058 |
| inclination: | 86.3939° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 299.9249° |
| argument of perigee: | 90.6049° |
| revolutions per day: | 14.34218249 |
| mean anomaly at epoch: | 269.5383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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