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 48401U 26145.25803296 +.00000000 +00000-0 +55591-4 0 00002
2 48401 53.1603 336.7770 0001350 63.1760 296.9380 15.31699886 05
| Epoch (UTC): | 25 May 2026 06:11:34 |
| Eccentricity: | 0.0001350 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 336.7770° |
| argument of perigee: | 63.1760° |
| revolutions per day: | 15.31699886 |
| mean anomaly at epoch: | 296.9380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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