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 51756U 26145.23760295 +.00000000 +00000-0 -14084-3 0 00000
2 51756 53.2141 325.4824 0001046 105.3907 254.7201 15.08850670 07
| Epoch (UTC): | 25 May 2026 05:42:08 |
| Eccentricity: | 0.0001046 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 325.4824° |
| argument of perigee: | 105.3907° |
| revolutions per day: | 15.08850670 |
| mean anomaly at epoch: | 254.7201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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