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 53686U 26145.41089130 +.00000000 +00000-0 -13412-2 0 00009
2 53686 97.4574 25.3074 0002701 63.7688 296.3816 15.05606497 03
| Epoch (UTC): | 25 May 2026 09:51:41 |
| Eccentricity: | 0.0002701 |
| inclination: | 97.4574° |
| perigee height: | 548 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 25.3074° |
| argument of perigee: | 63.7688° |
| revolutions per day: | 15.05606497 |
| mean anomaly at epoch: | 296.3816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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