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 37225U 26128.74634844 +.00000000 +00000-0 +66309-4 0 00009
2 37225 71.9724 247.4311 0017498 208.2202 151.8016 14.82100167 00
| Epoch (UTC): | 08 May 2026 17:54:44 |
| Eccentricity: | 0.0017498 |
| inclination: | 71.9724° |
| perigee height: | 610 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 247.4311° |
| argument of perigee: | 208.2202° |
| revolutions per day: | 14.82100167 |
| mean anomaly at epoch: | 151.8016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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