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 56787U 26145.38186928 +.00000000 +00000-0 +59405-4 0 00006
2 56787 69.9987 130.9960 0003414 265.8756 94.2013 14.98320696 09
| Epoch (UTC): | 25 May 2026 09:09:53 |
| Eccentricity: | 0.0003414 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 130.9960° |
| argument of perigee: | 265.8756° |
| revolutions per day: | 14.98320696 |
| mean anomaly at epoch: | 94.2013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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