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 53783U 26145.10650222 +.00000000 +00000-0 +94089-4 0 00009
2 53783 53.2133 290.9897 0001304 90.0306 270.0836 15.08830897 00
| Epoch (UTC): | 25 May 2026 02:33:21 |
| Eccentricity: | 0.0001304 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 290.9897° |
| argument of perigee: | 90.0306° |
| revolutions per day: | 15.08830897 |
| mean anomaly at epoch: | 270.0836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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