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 27640U 26069.96804682 +.00000000 +00000-0 +98758-4 0 00009
2 27640 98.7161 78.3418 0014812 133.0122 227.2299 14.19913224 01
| Epoch (UTC): | 10 March 2026 23:13:59 |
| Eccentricity: | 0.0014812 |
| inclination: | 98.7161° |
| perigee height: | 815 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 78.3418° |
| argument of perigee: | 133.0122° |
| revolutions per day: | 14.19913224 |
| mean anomaly at epoch: | 227.2299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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