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 48449U 26145.39726775 +.00000000 +00000-0 +27133-4 0 00006
2 48449 53.1580 181.3602 0001360 92.5549 267.5608 15.31695013 06
| Epoch (UTC): | 25 May 2026 09:32:03 |
| Eccentricity: | 0.0001360 |
| inclination: | 53.1580° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 181.3602° |
| argument of perigee: | 92.5549° |
| revolutions per day: | 15.31695013 |
| mean anomaly at epoch: | 267.5608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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