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 56066U 26145.26883742 +.00000000 +00000-0 -11541-3 0 00000
2 56066 87.9108 233.3228 0002769 92.3396 267.8052 13.16595660 09
| Epoch (UTC): | 25 May 2026 06:27:07 |
| Eccentricity: | 0.0002769 |
| inclination: | 87.9108° |
| perigee height: | 1196 km |
| apogee height: | 1200 km |
| right ascension of ascending node: | 233.3228° |
| argument of perigee: | 92.3396° |
| revolutions per day: | 13.16595660 |
| mean anomaly at epoch: | 267.8052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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