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 56427U 26145.24574884 +.00000000 +00000-0 +25041-4 0 00003
2 56427 43.0033 107.5576 0001111 265.6865 94.3859 15.27576843 08
| Epoch (UTC): | 25 May 2026 05:53:52 |
| Eccentricity: | 0.0001111 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.5576° |
| argument of perigee: | 265.6865° |
| revolutions per day: | 15.27576843 |
| mean anomaly at epoch: | 94.3859° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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