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 37779U 26145.59126846 +.00000000 +00000-0 +00000-0 0 00005
2 37779 0.6324 84.7827 0003389 330.2317 79.0197 1.00268135 07
| Epoch (UTC): | 25 May 2026 14:11:25 |
| Eccentricity: | 0.0003389 |
| inclination: | 0.6324° |
| perigee height: | 35773 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 84.7827° |
| argument of perigee: | 330.2317° |
| revolutions per day: | 1.00268135 |
| mean anomaly at epoch: | 79.0197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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