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 27847U 26106.97978307 +.00000000 +00000-0 +76808-4 0 00009
2 27847 98.6890 116.1788 0008897 349.5823 10.5170 14.23825947 07
| Epoch (UTC): | 16 April 2026 23:30:53 |
| Eccentricity: | 0.0008897 |
| inclination: | 98.6890° |
| perigee height: | 806 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 116.1788° |
| argument of perigee: | 349.5823° |
| revolutions per day: | 14.23825947 |
| mean anomaly at epoch: | 10.5170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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