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 37185U 26145.56093499 +.00000000 +00000-0 +00000-0 0 00000
2 37185 0.0625 273.5060 0003275 278.6796 137.7052 1.00272820 01
| Epoch (UTC): | 25 May 2026 13:27:44 |
| Eccentricity: | 0.0003275 |
| inclination: | 0.0625° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 273.5060° |
| argument of perigee: | 278.6796° |
| revolutions per day: | 1.00272820 |
| mean anomaly at epoch: | 137.7052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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