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 54858U 26145.13242486 +.00000000 +00000-0 +44684-4 0 00001
2 54858 43.0062 49.6944 0001350 271.1307 88.9390 15.27581139 02
| Epoch (UTC): | 25 May 2026 03:10:41 |
| Eccentricity: | 0.0001350 |
| inclination: | 43.0062° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 49.6944° |
| argument of perigee: | 271.1307° |
| revolutions per day: | 15.27581139 |
| mean anomaly at epoch: | 88.9390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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