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 55177U 26145.34024961 +.00000000 +00000-0 -11137-5 0 00004
2 55177 87.9154 10.4120 0001787 76.4094 283.7237 13.17650000 07
| Epoch (UTC): | 25 May 2026 08:09:57 |
| Eccentricity: | 0.0001787 |
| inclination: | 87.9154° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4120° |
| argument of perigee: | 76.4094° |
| revolutions per day: | 13.17650000 |
| mean anomaly at epoch: | 283.7237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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