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 51973U 26145.41815294 +.00000000 +00000-0 +17791-4 0 00009
2 51973 53.1611 40.0929 0001375 95.0240 265.0918 15.31701723 05
| Epoch (UTC): | 25 May 2026 10:02:08 |
| Eccentricity: | 0.0001375 |
| inclination: | 53.1611° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 40.0929° |
| argument of perigee: | 95.0240° |
| revolutions per day: | 15.31701723 |
| mean anomaly at epoch: | 265.0918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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