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 55490U 26145.35778273 +.00000000 +00000-0 +35350-4 0 00006
2 55490 43.0014 266.4838 0001607 258.9555 101.1116 15.27578845 00
| Epoch (UTC): | 25 May 2026 08:35:12 |
| Eccentricity: | 0.0001607 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.4838° |
| argument of perigee: | 258.9555° |
| revolutions per day: | 15.27578845 |
| mean anomaly at epoch: | 101.1116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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