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 55832U 26145.21975212 +.00000000 +00000-0 +18393-3 0 00000
2 55832 87.9174 309.5435 0002075 99.1459 260.9908 13.19720911 09
| Epoch (UTC): | 25 May 2026 05:16:26 |
| Eccentricity: | 0.0002075 |
| inclination: | 87.9174° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5435° |
| argument of perigee: | 99.1459° |
| revolutions per day: | 13.19720911 |
| mean anomaly at epoch: | 260.9908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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