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 37227U 26140.54354676 +.00000000 +00000-0 +57000-4 0 00003
2 37227 71.9660 197.6918 0014388 173.8294 186.3052 14.85203572 03
| Epoch (UTC): | 20 May 2026 13:02:42 |
| Eccentricity: | 0.0014388 |
| inclination: | 71.9660° |
| perigee height: | 603 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 197.6918° |
| argument of perigee: | 173.8294° |
| revolutions per day: | 14.85203572 |
| mean anomaly at epoch: | 186.3052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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