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 43072U 26145.47045294 +.00000000 +00000-0 -18269-4 0 00003
2 43072 86.3950 331.5031 0001765 83.3616 276.7780 14.34217741 02
| Epoch (UTC): | 25 May 2026 11:17:27 |
| Eccentricity: | 0.0001765 |
| inclination: | 86.3950° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 331.5031° |
| argument of perigee: | 83.3616° |
| revolutions per day: | 14.34217741 |
| mean anomaly at epoch: | 276.7780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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