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 48690U 26145.22758265 +.00000000 +00000-0 +62249-4 0 00002
2 48690 53.1596 79.3454 0001252 86.5887 273.5258 15.31705767 06
| Epoch (UTC): | 25 May 2026 05:27:43 |
| Eccentricity: | 0.0001252 |
| inclination: | 53.1596° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 79.3454° |
| argument of perigee: | 86.5887° |
| revolutions per day: | 15.31705767 |
| mean anomaly at epoch: | 273.5258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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