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 27940U 26040.50178060 +.00000000 +00000-0 +15921-3 0 00005
2 27940 98.3774 215.1192 0013793 43.3577 316.8710 14.69320412 03
| Epoch (UTC): | 09 February 2026 12:02:33 |
| Eccentricity: | 0.0013793 |
| inclination: | 98.3774° |
| perigee height: | 654 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 215.1192° |
| argument of perigee: | 43.3577° |
| revolutions per day: | 14.69320412 |
| mean anomaly at epoch: | 316.8710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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