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 26064.94904314 +.00000000 +00000-0 +15666-3 0 00004
2 27940 98.3808 240.1960 0012340 326.5285 33.5138 14.69360348 00
| Epoch (UTC): | 05 March 2026 22:46:37 |
| Eccentricity: | 0.0012340 |
| inclination: | 98.3808° |
| perigee height: | 654 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 240.1960° |
| argument of perigee: | 326.5285° |
| revolutions per day: | 14.69360348 |
| mean anomaly at epoch: | 33.5138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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