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 43790U 26145.10134337 +.00000000 +00000-0 +20632-3 0 00002
2 43790 97.4250 195.3831 0012686 69.7087 290.5507 15.12730541 09
| Epoch (UTC): | 25 May 2026 02:25:56 |
| Eccentricity: | 0.0012686 |
| inclination: | 97.4250° |
| perigee height: | 519 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 195.3831° |
| argument of perigee: | 69.7087° |
| revolutions per day: | 15.12730541 |
| mean anomaly at epoch: | 290.5507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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