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 65907U 26065.27358486 +.00000000 +00000-0 +15634-2 0 00003
2 65907 53.1625 27.0381 0001290 90.5855 269.5294 15.30253298 01
| Epoch (UTC): | 06 March 2026 06:33:57 |
| Eccentricity: | 0.0001290 |
| inclination: | 53.1625° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 27.0381° |
| argument of perigee: | 90.5855° |
| revolutions per day: | 15.30253298 |
| mean anomaly at epoch: | 269.5294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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