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 48775U 26145.38319041 +.00000000 +00000-0 +39109-3 0 00006
2 48775 87.8998 263.7288 0001636 99.2090 260.9226 13.15547218 07
| Epoch (UTC): | 25 May 2026 09:11:47 |
| Eccentricity: | 0.0001636 |
| inclination: | 87.8998° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7288° |
| argument of perigee: | 99.2090° |
| revolutions per day: | 13.15547218 |
| mean anomaly at epoch: | 260.9226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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