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 56300U 26145.03187291 +.00000000 +00000-0 +41468-4 0 00003
2 56300 43.0039 137.9386 0001367 277.1020 82.9676 15.27574552 09
| Epoch (UTC): | 25 May 2026 00:45:53 |
| Eccentricity: | 0.0001367 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 137.9386° |
| argument of perigee: | 277.1020° |
| revolutions per day: | 15.27574552 |
| mean anomaly at epoch: | 82.9676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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