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 64127U 26145.62917748 +.00000000 +00000-0 +12597-2 0 00001
2 64127 43.0007 229.7299 0004647 243.7771 116.2619 15.70860549 09
| Epoch (UTC): | 25 May 2026 15:06:00 |
| Eccentricity: | 0.0004647 |
| inclination: | 43.0007° |
| perigee height: | 353 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 229.7299° |
| argument of perigee: | 243.7771° |
| revolutions per day: | 15.70860549 |
| mean anomaly at epoch: | 116.2619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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