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 48374U 26145.58796215 +.00000000 +00000-0 +73466-4 0 00000
2 48374 53.1607 350.1261 0001285 89.1472 270.9677 15.31699855 05
| Epoch (UTC): | 25 May 2026 14:06:39 |
| Eccentricity: | 0.0001285 |
| inclination: | 53.1607° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 350.1261° |
| argument of perigee: | 89.1472° |
| revolutions per day: | 15.31699855 |
| mean anomaly at epoch: | 270.9677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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