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 55486U 26145.32579865 +.00000000 +00000-0 +14532-4 0 00003
2 55486 43.0059 267.0648 0001997 280.2108 79.8518 15.27575504 00
| Epoch (UTC): | 25 May 2026 07:49:09 |
| Eccentricity: | 0.0001997 |
| inclination: | 43.0059° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 267.0648° |
| argument of perigee: | 280.2108° |
| revolutions per day: | 15.27575504 |
| mean anomaly at epoch: | 79.8518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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