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 51751U 26145.61760412 +.00000000 +00000-0 +50298-4 0 00005
2 51751 53.2090 323.7878 0001019 72.0072 288.1031 15.08843160 06
| Epoch (UTC): | 25 May 2026 14:49:20 |
| Eccentricity: | 0.0001019 |
| inclination: | 53.2090° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 323.7878° |
| argument of perigee: | 72.0072° |
| revolutions per day: | 15.08843160 |
| mean anomaly at epoch: | 288.1031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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