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 51815U 26144.94136794 +.00000000 +00000-0 +25041-6 0 00001
2 51815 53.2137 346.8134 0001492 94.7947 265.3216 15.08841324 09
| Epoch (UTC): | 24 May 2026 22:35:34 |
| Eccentricity: | 0.0001492 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 346.8134° |
| argument of perigee: | 94.7947° |
| revolutions per day: | 15.08841324 |
| mean anomaly at epoch: | 265.3216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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