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 37794U 26077.87003006 +.00000000 +00000-0 +13480-3 0 00008
2 37794 97.8317 62.5953 0013515 96.4030 302.0970 14.65517652 07
| Epoch (UTC): | 18 March 2026 20:52:50 |
| Eccentricity: | 0.0013515 |
| inclination: | 97.8317° |
| perigee height: | 666 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 62.5953° |
| argument of perigee: | 96.4030° |
| revolutions per day: | 14.65517652 |
| mean anomaly at epoch: | 302.0970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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