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 43078U 26145.40994583 +.00000000 +00000-0 +74680-4 0 00004
2 43078 86.3940 299.9979 0002367 92.4898 267.6569 14.34219441 00
| Epoch (UTC): | 25 May 2026 09:50:19 |
| Eccentricity: | 0.0002367 |
| inclination: | 86.3940° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 299.9979° |
| argument of perigee: | 92.4898° |
| revolutions per day: | 14.34219441 |
| mean anomaly at epoch: | 267.6569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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