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 45429U 26145.41365605 +.00000000 +00000-0 +94307-3 0 00001
2 45429 87.8911 25.5975 0001952 78.8306 281.3041 13.11418118 00
| Epoch (UTC): | 25 May 2026 09:55:39 |
| Eccentricity: | 0.0001952 |
| inclination: | 87.8911° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5975° |
| argument of perigee: | 78.8306° |
| revolutions per day: | 13.11418118 |
| mean anomaly at epoch: | 281.3041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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