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 53468U 26145.58256262 +.00000000 +00000-0 -92731-4 0 00000
2 53468 97.4456 265.5410 0001055 132.5784 227.5532 15.05655841 03
| Epoch (UTC): | 25 May 2026 13:58:53 |
| Eccentricity: | 0.0001055 |
| inclination: | 97.4456° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 265.5410° |
| argument of perigee: | 132.5784° |
| revolutions per day: | 15.05655841 |
| mean anomaly at epoch: | 227.5532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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