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 55176U 26145.60523440 +.00000000 +00000-0 -96577-3 0 00007
2 55176 87.8912 25.5618 0001307 100.8074 259.3201 13.11414654 01
| Epoch (UTC): | 25 May 2026 14:31:32 |
| Eccentricity: | 0.0001307 |
| inclination: | 87.8912° |
| perigee height: | 1217 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5618° |
| argument of perigee: | 100.8074° |
| revolutions per day: | 13.11414654 |
| mean anomaly at epoch: | 259.3201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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