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 51783U 26145.29102134 +.00000000 +00000-0 +36131-3 0 00004
2 51783 53.2137 355.2929 0001529 98.8494 261.2671 15.08810645 04
| Epoch (UTC): | 25 May 2026 06:59:04 |
| Eccentricity: | 0.0001529 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 355.2929° |
| argument of perigee: | 98.8494° |
| revolutions per day: | 15.08810645 |
| mean anomaly at epoch: | 261.2671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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