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 64027U 26145.33979987 +.00000000 +00000-0 +26352-3 0 00006
2 64027 70.0002 281.1888 0002544 272.1424 87.9444 14.98338183 07
| Epoch (UTC): | 25 May 2026 08:09:18 |
| Eccentricity: | 0.0002544 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.1888° |
| argument of perigee: | 272.1424° |
| revolutions per day: | 14.98338183 |
| mean anomaly at epoch: | 87.9444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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