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 56549U 26145.00312094 +.00000000 +00000-0 +30080-4 0 00004
2 56549 43.0027 152.5748 0001287 290.7054 69.3660 15.27575985 08
| Epoch (UTC): | 25 May 2026 00:04:29 |
| Eccentricity: | 0.0001287 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 152.5748° |
| argument of perigee: | 290.7054° |
| revolutions per day: | 15.27575985 |
| mean anomaly at epoch: | 69.3660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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