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 48358U 26145.59069191 +.00000000 +00000-0 +53051-4 0 00007
2 48358 53.1608 0.4593 0001208 81.2149 278.8990 15.31691596 09
| Epoch (UTC): | 25 May 2026 14:10:35 |
| Eccentricity: | 0.0001208 |
| inclination: | 53.1608° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 0.4593° |
| argument of perigee: | 81.2149° |
| revolutions per day: | 15.31691596 |
| mean anomaly at epoch: | 278.8990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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