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 43074U 26145.48313731 +.00000000 +00000-0 +14308-4 0 00009
2 43074 86.3958 331.5550 0002112 89.2745 270.8693 14.34217813 01
| Epoch (UTC): | 25 May 2026 11:35:43 |
| Eccentricity: | 0.0002112 |
| inclination: | 86.3958° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 331.5550° |
| argument of perigee: | 89.2745° |
| revolutions per day: | 14.34217813 |
| mean anomaly at epoch: | 270.8693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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