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 65737U 26145.52065995 +.00000000 +00000-0 +72459-3 0 00000
2 65737 53.1606 336.2418 0001881 77.7526 282.3686 15.30218804 07
| Epoch (UTC): | 25 May 2026 12:29:45 |
| Eccentricity: | 0.0001881 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 336.2418° |
| argument of perigee: | 77.7526° |
| revolutions per day: | 15.30218804 |
| mean anomaly at epoch: | 282.3686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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