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 56731U 26145.65217647 +.00000000 +00000-0 +25919-3 0 00000
2 56731 40.9956 311.8341 0006024 130.9079 229.2268 15.40967662 06
| Epoch (UTC): | 25 May 2026 15:39:08 |
| Eccentricity: | 0.0006024 |
| inclination: | 40.9956° |
| perigee height: | 439 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 311.8341° |
| argument of perigee: | 130.9079° |
| revolutions per day: | 15.40967662 |
| mean anomaly at epoch: | 229.2268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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