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 37605U 26145.52337176 +.00000000 +00000-0 +00000-0 0 00006
2 37605 2.0748 82.0883 0002864 227.2350 177.2670 1.00270344 05
| Epoch (UTC): | 25 May 2026 12:33:39 |
| Eccentricity: | 0.0002864 |
| inclination: | 2.0748° |
| perigee height: | 35775 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 82.0883° |
| argument of perigee: | 227.2350° |
| revolutions per day: | 1.00270344 |
| mean anomaly at epoch: | 177.2670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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