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 51729U 26145.52372920 +.00000000 +00000-0 +25996-4 0 00000
2 51729 53.2147 334.1975 0001272 89.2759 270.8379 15.08837554 04
| Epoch (UTC): | 25 May 2026 12:34:10 |
| Eccentricity: | 0.0001272 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 334.1975° |
| argument of perigee: | 89.2759° |
| revolutions per day: | 15.08837554 |
| mean anomaly at epoch: | 270.8379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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