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 51779U 26145.29838243 +.00000000 +00000-0 +33844-3 0 00004
2 51779 53.2132 355.2570 0001255 94.2867 265.8268 15.08812397 04
| Epoch (UTC): | 25 May 2026 07:09:40 |
| Eccentricity: | 0.0001255 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 355.2570° |
| argument of perigee: | 94.2867° |
| revolutions per day: | 15.08812397 |
| mean anomaly at epoch: | 265.8268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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