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 26547U 26088.17995038 +.00000000 +00000-0 +55099-3 0 00004
2 26547 64.5466 10.4996 0037684 309.3641 50.4141 15.09185148 07
| Epoch (UTC): | 29 March 2026 04:19:07 |
| Eccentricity: | 0.0037684 |
| inclination: | 64.5466° |
| perigee height: | 513 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 10.4996° |
| argument of perigee: | 309.3641° |
| revolutions per day: | 15.09185148 |
| mean anomaly at epoch: | 50.4141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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