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 26037.62370692 +.00000000 +00000-0 +11085-3 0 00003
2 27640 98.7155 46.4898 0013228 226.0467 133.9619 14.19899891 09
| Epoch (UTC): | 06 February 2026 14:58:08 |
| Eccentricity: | 0.0013228 |
| inclination: | 98.7155° |
| perigee height: | 816 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 46.4898° |
| argument of perigee: | 226.0467° |
| revolutions per day: | 14.19899891 |
| mean anomaly at epoch: | 133.9619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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