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 51131U 26145.17965079 +.00000000 +00000-0 +29384-4 0 00006
2 51131 53.2146 315.7439 0001156 92.2626 267.8498 15.08834147 01
| Epoch (UTC): | 25 May 2026 04:18:41 |
| Eccentricity: | 0.0001156 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 315.7439° |
| argument of perigee: | 92.2626° |
| revolutions per day: | 15.08834147 |
| mean anomaly at epoch: | 267.8498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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