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 56476U 26145.10417642 +.00000000 +00000-0 -33054-4 0 00004
2 56476 69.9991 291.8578 0002783 254.3964 105.6888 14.98329351 07
| Epoch (UTC): | 25 May 2026 02:30:00 |
| Eccentricity: | 0.0002783 |
| inclination: | 69.9991° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 291.8578° |
| argument of perigee: | 254.3964° |
| revolutions per day: | 14.98329351 |
| mean anomaly at epoch: | 105.6888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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