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 51746U 26145.22384823 +.00000000 +00000-0 +17114-3 0 00003
2 51746 53.2138 325.5541 0001272 86.9715 273.1422 15.08831648 05
| Epoch (UTC): | 25 May 2026 05:22:20 |
| Eccentricity: | 0.0001272 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 325.5541° |
| argument of perigee: | 86.9715° |
| revolutions per day: | 15.08831648 |
| mean anomaly at epoch: | 273.1422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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