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 56393U 26145.34986890 +.00000000 +00000-0 -14195-4 0 00009
2 56393 43.0034 124.9712 0001398 253.0735 106.9964 15.27569561 06
| Epoch (UTC): | 25 May 2026 08:23:48 |
| Eccentricity: | 0.0001398 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.9712° |
| argument of perigee: | 253.0735° |
| revolutions per day: | 15.27569561 |
| mean anomaly at epoch: | 106.9964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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