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 43076U 26145.46410759 +.00000000 +00000-0 +13672-4 0 00000
2 43076 86.3961 331.6631 0001729 94.3593 265.7800 14.34218301 05
| Epoch (UTC): | 25 May 2026 11:08:18 |
| Eccentricity: | 0.0001729 |
| inclination: | 86.3961° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 331.6631° |
| argument of perigee: | 94.3593° |
| revolutions per day: | 14.34218301 |
| mean anomaly at epoch: | 265.7800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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