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 26073.46115492 +.00000000 +00000-0 +13474-3 0 00007
2 27940 98.3819 248.9296 0011987 297.8067 62.1922 14.69376189 03
| Epoch (UTC): | 14 March 2026 11:04:03 |
| Eccentricity: | 0.0011987 |
| inclination: | 98.3819° |
| perigee height: | 655 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 248.9296° |
| argument of perigee: | 297.8067° |
| revolutions per day: | 14.69376189 |
| mean anomaly at epoch: | 62.1922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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