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 48443U 26145.47648742 +.00000000 +00000-0 -55687-4 0 00002
2 48443 53.1581 180.9499 0001389 89.4656 270.6505 15.31697907 00
| Epoch (UTC): | 25 May 2026 11:26:08 |
| Eccentricity: | 0.0001389 |
| inclination: | 53.1581° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 180.9499° |
| argument of perigee: | 89.4656° |
| revolutions per day: | 15.31697907 |
| mean anomaly at epoch: | 270.6505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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