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 53475U 26145.66668980 +.00000000 +00000-0 +13687-1 0 00000
2 53475 97.6035 267.7697 0000857 81.4676 217.7598 15.43101949 08
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000857 |
| inclination: | 97.6035° |
| perigee height: | 436 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 267.7697° |
| argument of perigee: | 81.4676° |
| revolutions per day: | 15.43101949 |
| mean anomaly at epoch: | 217.7598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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