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 55281U 26145.44538400 +.00000000 +00000-0 -75461-4 0 00008
2 55281 69.9992 210.9055 0003385 270.9072 89.1699 14.98325214 06
| Epoch (UTC): | 25 May 2026 10:41:21 |
| Eccentricity: | 0.0003385 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 210.9055° |
| argument of perigee: | 270.9072° |
| revolutions per day: | 14.98325214 |
| mean anomaly at epoch: | 89.1699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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