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 43926U 26145.43795052 +.00000000 +00000-0 +73169-4 0 00000
2 43926 86.4244 34.7025 0002625 73.6641 286.4846 14.38608510 01
| Epoch (UTC): | 25 May 2026 10:30:38 |
| Eccentricity: | 0.0002625 |
| inclination: | 86.4244° |
| perigee height: | 761 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 34.7025° |
| argument of perigee: | 73.6641° |
| revolutions per day: | 14.38608510 |
| mean anomaly at epoch: | 286.4846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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