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 55488U 26145.37707512 +.00000000 +00000-0 +18753-3 0 00000
2 55488 43.0019 266.6336 0001386 296.4209 63.6500 15.27580962 06
| Epoch (UTC): | 25 May 2026 09:02:59 |
| Eccentricity: | 0.0001386 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.6336° |
| argument of perigee: | 296.4209° |
| revolutions per day: | 15.27580962 |
| mean anomaly at epoch: | 63.6500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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