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 56800U 26145.36124498 +.00000000 +00000-0 +42811-4 0 00007
2 56800 69.9983 151.1890 0003483 267.8044 92.2716 14.98331369 03
| Epoch (UTC): | 25 May 2026 08:40:11 |
| Eccentricity: | 0.0003483 |
| inclination: | 69.9983° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 151.1890° |
| argument of perigee: | 267.8044° |
| revolutions per day: | 14.98331369 |
| mean anomaly at epoch: | 92.2716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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