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 56804U 26145.38603926 +.00000000 +00000-0 -31094-4 0 00003
2 56804 69.9988 131.0078 0003357 267.6815 92.3959 14.98333888 09
| Epoch (UTC): | 25 May 2026 09:15:53 |
| Eccentricity: | 0.0003357 |
| inclination: | 69.9988° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 131.0078° |
| argument of perigee: | 267.6815° |
| revolutions per day: | 14.98333888 |
| mean anomaly at epoch: | 92.3959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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