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 37756U 26070.96774096 +.00000000 +00000-0 +74142-3 0 00005
2 37756 51.4392 359.8842 1812465 180.3702 179.5853 11.46816049 09
| Epoch (UTC): | 11 March 2026 23:13:32 |
| Eccentricity: | 0.1812465 |
| inclination: | 51.4392° |
| perigee height: | 423 km |
| apogee height: | 3434 km |
| right ascension of ascending node: | 359.8842° |
| argument of perigee: | 180.3702° |
| revolutions per day: | 11.46816049 |
| mean anomaly at epoch: | 179.5853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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