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 51737U 26145.56053251 +.00000000 +00000-0 +23841-4 0 00003
2 51737 53.2125 334.0339 0001252 93.8583 266.2552 15.08832918 07
| Epoch (UTC): | 25 May 2026 13:27:10 |
| Eccentricity: | 0.0001252 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 334.0339° |
| argument of perigee: | 93.8583° |
| revolutions per day: | 15.08832918 |
| mean anomaly at epoch: | 266.2552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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