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 55348U 26145.24438323 +.00000000 +00000-0 +16249-4 0 00001
2 55348 43.0024 230.8760 0001489 269.1494 90.9187 15.27575741 01
| Epoch (UTC): | 25 May 2026 05:51:54 |
| Eccentricity: | 0.0001489 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 230.8760° |
| argument of perigee: | 269.1494° |
| revolutions per day: | 15.27575741 |
| mean anomaly at epoch: | 90.9187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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