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 10677U 26041.91312014 +.00000000 +00000-0 +13755-3 0 00002
2 10677 74.0361 217.6091 0015663 236.1845 123.7821 14.41690133 06
| Epoch (UTC): | 10 February 2026 21:54:53 |
| Eccentricity: | 0.0015663 |
| inclination: | 74.0361° |
| perigee height: | 742 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 217.6091° |
| argument of perigee: | 236.1845° |
| revolutions per day: | 14.41690133 |
| mean anomaly at epoch: | 123.7821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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